Calculators Created by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore
https://www.linkedin.com/in/maiarutselvan-v-ba5533149/
301
Formulas Created
274
Formulas Verified
100
Across Categories

List of Calculators by Maiarutselvan V

Following is a combined list of all the calculators that have been created and verified by Maiarutselvan V. Maiarutselvan V has created 301 and verified 274 calculators across 100 different categories till date.
Verified Area of Composite Wall of 2 Layers
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Verified Inner Surface Temperature of Composite Wall for 2 Layers in Series
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Verified Thermal Resistance of Composite Wall with 2 Layers in Series
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5 More 2 Layers Calculators
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Verified Area of Composite Wall of 3 Layers
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Verified Inner Surface Temperature of Composite Wall of 3 Layers in Series
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Verified Length of 3rd Layer of Composite Wall in Conduction through Walls
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Verified Thermal Resistance of Composite Wall with 3 Layers in Series
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2 More 3 Layers Calculators
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Verified Aerodynamic Heating to Surface
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Verified Chapman-Rubesin Factor
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Verified Coefficient of Friction using Stanton Equation for Incompressible Flow
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Verified Density Calculation using Chapman-Rubesin Factor
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Verified Stanton Number for Incompressible Flow
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Verified Static Density Calculation using Chapman-Rubesin Factor
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Verified Static Viscosity Calculation using Chapman-Rubesin Factor
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Verified Thermal Conductivity using Prandtl Number
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Verified Viscosity Calculation using Chapman-Rubesin Factor
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7 More Aero Thermal Dynamics Calculators
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Verified Airspeed Measurement by Venturi
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Verified Dynamic Pressure in Incompressible Flow
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Verified Test Section Velocity by Manometric Height for Wind Tunnel
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Verified Total Pressure in Incompressible Flow
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Verified Wind Tunnel Pressure Difference by Manometer
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Verified Wind Tunnel Test Section Velocity
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4 More Aerodynamic Measurements and Wind Tunnel Testing Calculators
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Verified Sideslip Angle for Aircraft
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10 More Aerodynamic Parameters Calculators
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Verified Normal Force Coefficient with Aerodynamic Normal Force
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Verified Rolling Moment
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Verified Rolling moment coefficient
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Verified Velocity along Pitch Axis for Small Sideslip Angle
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Verified Velocity along Roll Axis for Small Angle of Attack
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13 More Aircraft Dynamics Nomenclature Calculators
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Verified Current Gain of Amplifier in Decibels
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20 More Amplifier Characteristics Calculators
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Verified Non-Dimensional Pressure
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Verified Non-Dimensional Pressure for High Mach Number
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Verified Slenderness Ratio with Cone Radius for Hypersonic Vehicle
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8 More Approximate Methods of Hypersonic Inviscid Flowfields Calculators
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Verified Coefficient of Drag over Flat under Freestream Flow Conditions
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Verified Drag Force over Flat Plate
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Verified Freestream Stanton Number for Flat Plate
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Verified Local Heat Transfer over Flat Plate using Stanton Number
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Verified Pressure Ratio for Insulated Flat Plate, Weak Interaction
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10 More Approximate Results Applied to Hypersonic Vehicles Calculators
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Verified Pressure Coefficient for Blast Wave Theory
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5 More Blast Wave Part Theory Calculators
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Verified Acceleration of System given Mass of Body A
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Verified Acceleration of System given Mass of Body B
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Verified Frictional Force on Body B
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Verified Tension in String given Mass of Body A
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Verified Tension in String given Mass of Body B
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1 More Body Lying on Rough Inclined Plane Calculators
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Verified Coefficient of Friction given Frictional Force
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Verified Frictional Force
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5 More Body Lying on Rough Inclined Plane Calculators
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Verified Angle of Inclination of Plane with Body A
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Verified Angle of Inclination of Plane with Body B
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2 More Body Lying on Smooth Inclined Plane Calculators
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Verified Tension in String when One Body is Lying on Smooth Inclined Plane
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3 More Body Lying on Smooth Inclined Plane Calculators
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Created Area of Surface for Average Drag Coefficient
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Created Average Coefficient of Drag for Drag Force
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Created Coefficient of Drag for Blasius's Solution
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Created Coefficient of Drag for Reynold Number
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Created Distance from Leading Edge
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Created Distance from Leading Edge for Blasius's Solution
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Created Drag Force for Average Drag Coefficient
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Created Drag Force on Plate
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Created Freestream Velocity for Local Drag Coefficient
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Created Length of Plate for Reynold Number
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Created Local Drag Coefficient for Shear Stress
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Created Reynold Number at End of Plate
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Created Reynold Number for Drag Coefficient in Blasius's Solution
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Created Reynold Number for Drag Force on Plate
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Created Shear Stress at Boundary for Turbulent Boundary Layer over Flat Plate
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Created Shear Stress for Local Drag Coefficient
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Created Thickness of Boundary Layer
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Created Thickness of Boundary Layer for Blasius's Solution
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Created Velocity of Fluid for Reynold Number
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Created Viscosity of Liquid for Drag Force on Plate
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Created Width of Plate for Drag Force on Plate
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Created Angle of heel for metacentric height in experimental method
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Created Centre of Buoyancy
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Created Meta-centric height for time period of oscillation and radius of gyration
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Created Meta-centric height in experimental method
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Created Movable weight for metacentric height in experimental method
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Created Radius of gyration for metacentric height and time period of oscillation
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Created Time Period of Oscillation of Ship
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Created Volume of body in fluid for metacentric height and BG
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Created Volume of fluid displaced
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2 More Buoyancy Calculators
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Verified Thrust available for given excess power
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15 More Climbing Flight Calculators
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Created Bulk Modulus for Velocity of Sound Wave
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Created Mach Angle for Compressible Fluid Flow
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Created Mach Number for Compressible Fluid Flow
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Created Pressure Ratio for Maximum Flow Rate through Nozzle
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Created Velocity at Outlet of Nozzle for Maximum Flow Rate of Fluid
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Created Velocity of Projectile of Mach Cone in Compressible Fluid Flow
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Created Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
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Created Velocity of Sound Wave given Bulk Modulus
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Created Velocity of Sound Wave given Mach Number for Compressible Fluid Flow
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1 More Compressible Flow Parameters Calculators
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Verified Emissivity
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Verified Reference Viscosity
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9 More Computational Fluid Dynamic Solutions Calculators
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Verified Convection Resistance for Cylindrical Layer
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Verified Length of Cylindrical Wall for given Heat Flow Rate
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14 More Conduction in Cylinder Calculators
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Verified Convection Resistance for Spherical Layer
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Verified Heat Flow Rate through Spherical Composite Wall of 2 Layers in Series
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Verified Inner Surface Temperature of Spherical Wall
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Verified Outer Surface Temperature of Spherical Wall
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Verified Thermal Resistance of Spherical Composite Wall of 2 Layers in Series with Convection
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Verified Thickness of Spherical Wall to Maintain given Temperature Difference
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Verified Total Thermal Resistance of Spherical Wall of 2 Layers without Convection
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Verified Total Thermal Resistance of Spherical wall of 3 Layers without Convection
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Verified Total Thermal Resistance of Spherical Wall with Convection on Both Side
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2 More Conduction in Sphere Calculators
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Created Cutting Force for Frictional Force along Tool Rake Face and Thrust Force
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Created Cutting Force given Shear Force and Thrust Force
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4 More Cutting Force Calculators
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Created Circulation for Lift Force on Cylinder
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Created Length of Cylinder for Lift Force on Cylinder
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Created Location of Stagnation points for Rotating Cylinder in Uniform Flow Field
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Created Radius of Cylinder for location of Stagnation Points
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Created Radius of Cylinder for Single Stagnation Point
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2 More Cylinder Properties Calculators
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Verified Simplified Pressure Ratio for Blunt Cylinder Blast Wave
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7 More Cylindrical Blast Wave Calculators
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Verified Nusselt's Number with Reynolds Number, Stanton Number and Prandtl Number
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Verified Prandtl Number with Reynolds Number, Nusselt's Number, and Stanton Number
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2 More Dimensionless Quantities Calculators
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Created Diameter of Pipe for Difference in Pressure in Viscous Flow
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Created Diameter of Pipe for Head Loss due to Friction in Viscous Flow
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Created Diameter of Pipe for Loss of Pressure Head in Viscous Flow
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Created Diameter of Pipe from Maximum Velocity and Velocity at Any Radius
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Created Diameter of Shaft for Speed and Shear Stress of Fluid in Journal Bearing
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Created Diameter of Shaft for Torque Required in Foot-Step Bearing
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Created Diameter of Sphere in Falling Sphere Resistance Method
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Created External or Outer Radius of Collar for Total Torque
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Created Internal or Inner Radius of Collar for Total Torque
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Created Length for Difference of Pressure in Viscous Flow between Two Parallel Plates
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Created Length for Pressure Head Loss in Viscous Flow between Two Parallel Plates
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Created Length of Pipe for Difference of Pressure in Viscous Flow
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Created Length of Pipe for Head Loss due to Friction in Viscous Flow
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Created Length of Pipe for Loss of Pressure Head in Viscous Flow
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Created Length of Tube in Capillary Tube Method
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Created Radius of Capillary Tube
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Created Thickness of Oil Film for Shear Force in Journal Bearing
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Created Thickness of Oil Film for Speed and Diameter of Shaft in Journal Bearing
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Created Thickness of Oil Film for Torque required in Foot-Step Bearing
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Created Coefficient of Discharge for Time Required to Empty Reservoir
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Created Discharge over Broad-Crested Weir
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Created Discharge over Broad-Crested Weir for Head of Liquid at Middle
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Created Discharge over Broad-Crested Weir with Velocity of Approach
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Created Discharge over Rectangle Notch or Weir
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Created Discharge over Rectangle Weir Considering Bazin's formula
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Created Discharge over Rectangle Weir Considering Francis's formula
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Created Discharge over Rectangle Weir for Bazin's formula with Velocity of Approach
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Created Discharge over Rectangle Weir with Two End Contractions
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Created Discharge over Trapezoidal Notch or Weir
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Created Discharge over Triangular Notch or Weir
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Created Discharge with Velocity of Approach
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Created Discharge without Velocity of Approach
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Created Head of Liquid above V-notch
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Created Head of Liquid at Crest
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Created Time Required to Empty Reservoir
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Created Time Required to Empty Tank with Triangular Weir or Notch
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Verified Stream Function for 2-D Doublet Flow
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1 More Doublet Flow Calculators
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Verified Density behind Normal Shock given Upstream Density and Mach Number
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Verified Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
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Verified Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
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Verified Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
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11 More Downstream Shock Waves Calculators
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Created Area of body for Lift Force in body moving on Fluid
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Created Coefficient of drag for sphere in Oseen formula when Reynolds number is between 0.2 and 5
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Created Coefficient of drag for sphere in stoke's law when Reynolds number is less than 0.2
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Created Drag Force for body moving in Fluid of Certain Density
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Created Pressure Drag from Total Drag Force on Sphere
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Created Skin Friction Drag from Total Drag Force on Sphere
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Created Total Drag force on Sphere
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4 More Drag and Forces Calculators
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Verified Emissivity per Unit Mole
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Verified Kinetic Energy per Mole
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Verified Kinetic Energy per Mole using Molar Volume
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Verified Kinetic Energy per Mole using Temperature of Gas
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Verified Mean Free Path of Single-Species Gas
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Verified Pressure using Kinetic Energy per Mole
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Verified Pressure using Molar Volume
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Verified Specific Gas Constant using Kinetic Energy per Mole
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Verified Temperature of Gas using Emissivity per Unit Mole
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Verified Temperature of Gas using Kinetic Energy per Mole
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5 More Elements of Kinetic Theory Calculators
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Verified Forward Mach Angle of Expansion Fan
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Verified Pressure Ratio across Expansion Fan
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Verified Temperature Ratio across Expansion Fan
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7 More Expansion Waves Calculators
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Created Difference of Pressure for Viscous Flow between Two Parallel Plates
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Created Difference of Pressure for Viscous or Laminar Flow
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Created Loss of Head Due to Friction
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Created Loss of Pressure Head for Viscous Flow between Two Parallel Plates
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Created Loss of Pressure Head for Viscous Flow through Circular Pipe
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Created Power Absorbed in Collar Bearing
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Created Power Absorbed in Foot-Step Bearing
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Created Power Absorbed in Overcoming Viscous Resistance in Journal Bearing
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Created Viscosity of Fluid or Oil for Capillary Tube Method
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Created Viscosity of Fluid or Oil for Movement of Piston in Dash-Pot
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Created Viscosity of Fluid or Oil in Falling Sphere Resistance Method
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Created Viscosity of Fluid or Oil in Rotating Cylinder Method
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1 More Flow Analysis Calculators
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Created Absolute pressure head at constant head and atmospheric pressure head
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Created Atmospheric pressure head at constant head and absolute pressure head
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Created Head of Liquid above Centre of Orifice
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Created Head of liquid for head loss and coefficient of velocity
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Created Loss of head due to fluid resistance
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Created Loss of head due to sudden enlargement
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Created Area of Flow for Circular Channel
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Created Bazin's constant
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Created Chezy's constant considering Bazin formula
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Created Chezy's constant considering Kutter's formula
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Created Chezy's constant considering Manning's formula
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Created Chezy's constant considering velocity
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Created Critical depth considering flow in open channels
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Created Critical depth considering minimum specific energy
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Created Critical Depth using Critical Velocity
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Created Critical velocity considering flow in open channels
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Created Discharge per unit width considering flow in open channels
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Created Hydraulic mean depth considering Bazin formula
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Created Hydraulic mean depth considering Manning's formula
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Created Hydraulic mean depth using Chezy's formula
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Created Manning's coefficient or constant
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Created Minimum Specific Energy using Critical Depth
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Created Radius of Circular Channel using Wetted Perimeter
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Created Velocity of Chezy's formula
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Created Wetted Perimeter for Circular Channel
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Verified Boundary Layer Thickness for Laminar Flow
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Verified Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory
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6 More Flow over Airfoils Calculators
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Created Coefficient of discharge
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Created Coefficient of discharge for area and velocity
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Created Coefficient of Discharge given Time for Emptying Tank
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Created Coefficient of Discharge given Time of Emptying Circular Horizontal Tank
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Created Coefficient of Discharge given Time of Emptying Hemispherical Tank
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Created Discharge in Borda's Mouthpiece Running Free
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Created Discharge in Borda's Mouthpiece Running Full
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Created Discharge in Convergent-Divergent Mouthpiece
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Created Discharge through fully sub-merged orifice
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Created Discharge through large rectangular orifice
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Created Discharge through partially sub-merged orifice
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Created Coefficient of contraction for sudden contraction
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Created Discharge in Equivalent Pipe
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Created Retarding force for gradual closure of valves
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Created Time required to close Valve for Gradual Closure of Valves
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Created Time taken by pressure wave to travel
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Created Velocity at Outlet for Head Loss at Exit of Pipe
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Created Velocity at section 1-1 for sudden enlargement
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Created Velocity at section 2-2 for sudden contraction
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Created Velocity at section 2-2 for sudden enlargement
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Created Velocity of Flow at Outlet of Nozzle
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Created Velocity of Flow at outlet of Nozzle for Efficiency and Head
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Created Velocity of Fluid for Head Loss due to Obstruction in Pipe
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Created Velocity of fluid in pipe for head loss at entrance of pipe
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Created Velocity of liquid at vena-contracta
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3 More Flow Regime Calculators
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Created Angular Speed of Outer Cylinder in Rotating Cylinder Method
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Created Buoyant Force in Falling Sphere Resistance Method
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Created Density of Fluid in Falling Sphere Resistance Method
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Created Discharge in Capillary Tube Method
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Created Drag Force in Falling Sphere Resistance Method
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Created Maximum Velocity at any Radius using Velocity
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Created Rotational Speed considering Power Absorbed and Torque in Journal Bearing
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Created Rotational Speed for Torque Required in Collar Bearing
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Created Rotational Speed for Torque Required in Foot-Step Bearing
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Created Shear Force for Torque and Diameter of Shaft in Journal Bearing
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Created Shear Force or Viscous Resistance in Journal Bearing
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Created Shear Stress in Fluid or Oil of Journal Bearing
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Created Speed of Rotation for Shear Force in Journal Bearing
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Created Torque Required Considering Power Absorbed in Journal Bearing
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Created Torque Required to Overcome Shear Force in Journal Bearing
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Created Torque Required to Overcome Viscous Resistance in Collar Bearing
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Created Torque Required to Overcome Viscous Resistance in Foot-Step Bearing
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Created Total Torque Measured by Strain in Rotating Cylinder Method
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Created Velocity at Any Radius given Radius of Pipe, and Maximum Velocity
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Created Velocity of Piston or Body for Movement of Piston in Dash-Pot
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Created Velocity of Sphere in Falling Sphere Resistance Method
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Created Freestream Velocity for Lift Coefficient in Rotating Cylinder with Circulation
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Created Freestream velocity for lift coefficient with tangential speed
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Created Freestream Velocity for single Stagnation Point
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Created Tangential velocity for single stagnation point
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5 More Fluid Parameters and Characteristics Calculators
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Created Force along shear force for given force normal to shear force, shear, friction and normal rake angle
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Created Force along Shear Force given Cutting Force and Thrust Force
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1 More Force Along Shear Calculators
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Created Force normal to shear force for given cutting force, thrust force, and shear angle
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3 More Force Normal to Shear Calculators
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Created Frictional force along tool rake face for given cutting and thrust forces, normal rake angle
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5 More Forces and Friction Calculators
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Created Length of Crest of Weir or Notch
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Created Length of Section for Discharge over Rectangle Notch or Weir
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Created Length of Weir Considering Bazin's formula with Velocity of Approach
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Created Length of Weir Considering Bazin's formula without Velocity of Approach
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Created Length of Weir Considering Francis's formula
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Created Length of Weir for Broad-Crested Weir and Head of Liquid at Middle
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Created Length of Weir for Broad-Crested Weir with Velocity of Approach
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Created Length of Weir for Discharge over Broad-Crested Weir
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Created Length of Weir or Notch for Velocity of Approach
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Created Length of Weir or Notch without Velocity of Approach
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Created Area at vena contracta for discharge and constant head
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Created Area of Mouthpiece in Borda's Mouthpiece Running Free
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Created Area of Mouthpiece in Borda's Mouthpiece Running Full
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Created Area of Orifice given Time of Emptying Hemispherical Tank
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Created Area of Tank given Time for Emptying Tank
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Created Coefficient of Contraction given Area of Orifice
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Created Horizontal distance for coefficient of velocity and vertical distance
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Created Vertical distance for coefficient of velocity and horizontal distance
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Created Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle
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Created Area of Pipe for Maximum Power Transmission through Nozzle
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Created Diameter of Equivalent Pipe
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Created Diameter of nozzle for maximum power transmission through nozzle
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Created Length of Equivalent Pipe
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Created Length of pipe for maximum power transmission through nozzle
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Created Maximum Area of Obstruction in Pipe
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Created Feed Force
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Created Radial Force
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Created Side Cutting Edge Angle for Orthogonal Cutting
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Created Side Rake Angle for Orthogonal Cutting
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6 More Geometry of Turning Process Calculators
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Verified Glide angle for given lift-to-drag ratio
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5 More Gliding Flight Calculators
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Verified Ratio of Stagnation and Static Pressure
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17 More Governing Equations and Sound Wave Calculators
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Verified Load factor for given turn radius for high-performance fighter aircraft
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Verified Turn radius for high load factor
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Verified Turn Rate for given Lift Coefficient
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Verified Velocity for given pull-up maneuver rate
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Verified Velocity given Turn Radius for High Load Factor
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12 More High Load Factor Maneuver Calculators
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Verified Pressure Ratio of Blunt-Nosed Cylinder (First Approximation)
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Verified Radial Coordinate of Blunt-Nosed Cylinder (First Approximation)
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Verified Radius for Cylinder-Wedge Body Shape
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Verified Radius for Sphere-Cone Body Shape
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5 More Hypersonic Flight Paths Velocity of Altitude Map Calculators
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Verified Change in Velocity for Hypersonic Flow in X Direction
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Verified Coefficient of Pressure with Slenderness Ratio and Similarity Constant
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Verified Constant G used for Finding Location of Perturbed Shock
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Verified Density Ratio with Similarity Constant having Slenderness Ratio
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Verified Distance from Tip of Leading Edge to Base
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Verified Non Dimensionalised Time
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11 More Hypersonic Flow and Disturbances Calculators
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Verified Dynamic Viscosity around Wall
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Verified Local Shear Stress at Wall
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Verified Static Density Equation using Skin Friction Coefficient
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Verified Static Velocity Equation using Skin Friction Coefficient
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Verified Static Viscosity Relation using Temperature of Wall
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2 More Hypersonic Flow Parameters Calculators
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Verified Mach Ratio at High Mach Number
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Verified Pressure Ratio for High Mach Number
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Verified Pressure Ratio having High Mach Number with Similarity Constant
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17 More Hypersonic Flow Parameters Calculators
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Verified Boundary-Layer Momentum Thickness using Reynolds Number at Transition Point
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Verified Eddy Viscosity Calculation
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Verified Local Mach Number using Reynolds Number Equation at Transition Region
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Verified Location of Transition Point
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Verified Prandtl Number of Transition Flow
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Verified Specific Heat at Constant Pressure for Transient Flow
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Verified Static Density at Transition Point
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Verified Static Density Equation using Boundary-Layer Momentum Thickness
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Verified Static Velocity at Transition Point
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Verified Static Velocity using Boundary-Layer Momentum Thickness
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Verified Static Viscosity at Transition Point
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Verified Static Viscosity Equation using Boundary-Layer Momentum Thickness
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Verified Transition Reynolds Number
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3 More Hypersonic Transition Calculators
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Created Dimensions of Rankine half-body
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Created Distance of stagnation point S from source in flow past half body
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Created Location of stagnation point on x-axis
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Created Radial velocity at any radius
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Created Radius at any point considering radial velocity
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Created Radius of Rankine circle
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Created Stream function at point
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Created Stream Function at Point in Combined Flow
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Created Stream function in sink flow for angle
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Created Strength of doublet for stream function
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Created Strength of source for radial velocity and at any radius
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Created Strength of source for Rankine half body
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Created Uniform flow velocity for Rankine half body
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Created Uniform flow velocity for stream function at point in combined flow
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9 More Incompressible Flow Characteristics Calculators
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Created Actual Discharge in Venturimeter
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Created Angular Velocity of Vortex using Depth of Parabola
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Created Coefficient of pitot-tube for velocity at any point
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Created Depth of Parabola formed at Free Surface of Water
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Created Difference in Pressure Head for heavier Liquid in Manometer
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Created Difference in pressure head for light liquid in manometer
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Created Height or depth of paraboloid for volume of air
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Created Rate of flow or discharge
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Created Resultant bend force along x and y direction
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Created Resultant velocity for two velocity components
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Created Total Pressure Force at Bottom of Cylinder
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Created Total pressure force on top of cylinder
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Created Velocity at any point for coefficient of pitot-tube
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4 More Kinematics of Flow Calculators
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Verified Freestream Density by Kutta-Joukowski Theorem
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Verified Freestream Velocity by Kutta-Joukowski Theorem
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2 More Kutta Joukowski Lift Theorem Calculators
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Verified Newtonian Dynamic Pressure
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Verified Newtonian Pressure Distribution over Surface using Cosine Angle
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Verified Nusselt Number at Stagnation Point
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Verified Nusselt Number for Stagnation Point on Blunt Body
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Verified Stagnation Pressure
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2 More Laminar Boundary Layer at Stagnation point on Blunt body Calculators
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Verified Touchdown velocity
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4 More Landing Calculators
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Verified Aircraft forward velocity for given normal component of side velocity
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Verified Aircraft sideslip velocity for given dihedral angle
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Verified Dihedral angle for given sideslip velocity
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Verified Normal component of aircraft side velocity for given dihedral angle
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Verified Normal component of aircraft side velocity for given forward velocity
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Created Angle of Attack for Circulation developed on Airfoil
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Created Angle of Attack for Lift Coefficient on Airfoil
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Created Chord Length for Circulation developed on Airfoil
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Created Circulation developed on Airfoil
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Created Circulation for Single Stagnation Point
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Created Circulation in Location of Stagnation Points
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Created Coefficient of Lift for Airfoil
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Created Lift coefficient for lift force in body moving on fluid
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Created Lift Coefficient for Rotating Cylinder with Circulation
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Created Lift Coefficient for Rotating Cylinder with Tangential Speed
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Created Lift Force for body moving in Fluid of Certain Density
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Created Lift Force on Cylinder for Circulation
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Created Radius of Cylinder for Lift Coefficient in Rotating Cylinder with Circulation
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Created Tangential Velocity of Cylinder with Lift Coefficient
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Created Velocity of Airfoil for Circulation developed on Airfoil
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1 More Lift and Circulation Calculators
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Verified Coefficient of Lift for given thrust and weight
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Verified Lift Coefficient given Minimum required Thrust
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Verified Lift-to-Drag Ratio given required Thrust of Aircraft
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Verified Total Drag Force given required Power
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Verified Zero-lift drag coefficient at minimum required thrust
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Verified Zero-Lift Drag Coefficient given required Thrust
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13 More Lift and Drag Requirements Calculators
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Verified 2-D Lift Coefficient for Cylinder
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Verified Stream Function for Lifting Flow over Circular Cylinder
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8 More Lifting Flow over Cylinder Calculators
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Verified Local Heat Transfer Rate Calculation using Stanton Number
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Verified Local Heat Transfer Rate using Nusselt's Number
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Verified Stanton Number for Hypersonic Vehicle
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Verified Static Density Equation using Stanton Number
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Verified Static Velocity using Stanton Number
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Verified Thermal Conductivity at Edge of Boundary Layer Equation using Nusselt's Number
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3 More Local Heat Transfer for Hypersonic Flow Calculators
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Created Absolute Temperature for Velocity of Sound Wave in Isothermal Process
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Created Absolute Temperature for Velocity of Sound Wave using Adiabatic Process
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Created Density of Fluid considering Velocity at Outlet of Orifice
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Created Pressure at Inlet considering Maximum Flow Rate of Fluid
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Created Pressure at Inlet of Tank or Vessel considering Compressible Fluid Flow
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Created Velocity of Sound Wave using Adiabatic Process
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Created Velocity of Sound Wave using Isothermal Process
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Verified Coefficient of Drag Equation with Coefficient of Normal Force
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Verified Exact Normal Shock Wave Maximum Coefficient of Pressure
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Verified Force Exerted on Surface given Static Pressure
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Verified Mass Flux Incident on Surface Area
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Verified Maximum Pressure Coefficient
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9 More Newtonian Flow Calculators
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Verified Tangential Velocity for Non-Lifting Flow over Circular Cylinder
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9 More Nonlifting Flow over Cylinder Calculators
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Verified Component of Downstream Mach Number Normal to Oblique Shock for given Normal Upstream Mach Number
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Verified Density behind Oblique Shock for given Upstream Density and Normal Upstream Mach Number
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Verified Density Ratio across Oblique Shock
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Verified Pressure behind Oblique Shock for given Upstream Pressure and Normal Upstream Mach Number
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Verified Pressure Ratio across Oblique Shock
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Verified Temperature behind Oblique Shock for given Upstream Temperature and Normal Upstream Mach Number
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Verified Temperature Ratio across Oblique Shock
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3 More Oblique Shock Calculators
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Verified Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
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Verified Perpendicular Upstream Flow Components behind Shock Wave
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13 More Oblique Shock Relation Calculators
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Verified Friction Coefficient
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20 More Others and Extra Calculators
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Verified Energy for Blast Wave
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Verified Radial Coordinate of Blunt Slab Blast Wave
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Verified Time Required for Blast Wave
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5 More Planar and Blunt Slab Blast Wave Calculators
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Created Efficiency of power transmission in flow through pipes
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Created Efficiency of Power Transmission through Nozzle
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Created Efficiency of power transmission through nozzle for velocity and total head
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Created Power Lost ue to Sudden Enlargement
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Created Power transmission through pipes
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Verified Power required at Altitude
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Verified Power required at Altitude given Power at sea-level
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15 More Preliminary Aerodynamics Calculators
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Created Difference in liquid level in three compound pipes with same friction coefficient
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Created Head available at Base of Nozzle
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Created Head Loss due to Friction for Efficiency of Power Transmission
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Created Intensity of pressure wave produced for gradual closure of valves
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Created Loss of Head at Entrance of Pipe
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Created Loss of head at exit of pipe
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Created Loss of Head due to Bend in Pipe
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Created Loss of Head due to Obstruction in Pipe
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Created Loss of Head due to Sudden Contraction
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Created Loss of head due to sudden enlargement at any particular section of pipe
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Created Loss of head in equivalent pipe
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Created Total head at inlet of pipe for head available at base of nozzle
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Created Total head available at inlet of pipe for efficiency of power transmission
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1 More Pressure and Flow Head Calculators
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Verified Endurance of Propeller-Driven Airplane
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Verified Power Available for Reciprocating Engine-Propeller Combination
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Verified Propeller Efficiency for given Endurance of Propeller-Driven Airplane
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Verified Propeller Efficiency for given Range and Lift-to-Drag Ratio of Propeller-Driven Airplane
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Verified Propeller Efficiency for given Range of Propeller-Driven Airplane
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Verified Propeller Efficiency for Reciprocating Engine-Propeller Combination
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Verified Range of Propeller-Driven Airplane
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Verified Range of Propeller-Driven Airplane for given lift-to-drag ratio
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Verified Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
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Verified Specific Fuel Consumption for given Range and Lift-to-Drag Ratio of Propeller-Driven Airplane
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Verified Specific Fuel Consumption for given Range of Propeller-Driven Airplane
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11 More Propeller Driven Airplane Calculators
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Verified Static Enthalpy Ratio across Normal Shock
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Verified Temperature Ratio across Normal Shock
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4 More Property Change Across Shock Waves Calculators
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Verified Load Factor given Pull-Down Maneuver Radius
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Verified Load Factor given Pull-Up Maneuver Rate
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Verified Pull-down maneuver radius
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Verified Pull-Up Maneuver Rate
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Verified Velocity for given Pull-Down Maneuver Rate
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Verified Velocity for given Pull-Up Maneuver Radius
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6 More Pull Up and Pull Down Maneuver Calculators
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Verified Chord Length for Flat Plate Case
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Verified Local Reynolds Number
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Verified Mach Number at Reference Temperature
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Verified Overall Skin-Friction Drag Coefficient for Incompressible Flow
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Verified Reference Temperature Equation
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Verified Stanton Number Obtained from Classical Theory
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Verified Static Viscosity of Plate using Chord Length for Flat Plate Case
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Verified Wall Temperature using Reference Temperature
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7 More Reference Temperature Method Calculators
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Verified Detachment Distance of Cylinder Wedge Body Shape
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Verified Detachment Distance of Sphere Cone Body Shape
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Verified Grid Point Calculation for Shock Waves
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Verified Nose Radius of Cylinder-Wedge
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Verified Nose Radius of Sphere Cone
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Verified Pressure Ratio for Unsteady Waves
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Verified Ratio of New and Old Temperature
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3 More Shock Dynamics and Aerodynamic Shape Calculators
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Verified Inner Surface Temperature of Plane Wall
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Verified Temperature at Distance x from Inner Surface in Wall
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Verified Thermal Resistance of Wall
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5 More Single Plane Wall Calculators
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Verified Radial Velocity for 2-D Incompressible Source Flow
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Verified Stream Function for Semi-Infinite Body
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5 More Source Flow Calculators
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Verified Coefficient of Pressure Equation using Specific Heat Ratio
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Verified Curvilinear Grid Location Equation
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Verified Density Equation using Enthalpy and Pressure
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Verified Enthalpy Equation using Pressure and Density
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Verified Pressure Equation using Enthalpy and Density
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6 More Space Marching Finite Difference Method Additional Solutions of the Euler Equations Calculators
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Created Density of Fluid for Stagnation considering Compressible Fluid Flow
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Created Stagnation Density considering other Stagnation Properties of Fluid
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Created Stagnation Density given Compressible Fluid Flow
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Created Stagnation Pressure considering other Stagnation Properties of Fluid
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Created Stagnation Pressure for Compressible Fluid Flow
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Created Stagnation Temperature considering Compressible Fluid Flow
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Created Stagnation Temperature considering other Stagnation Properties of Fluid
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Created Temperature of Fluid for Stagnation Temperature considering Compressible Fluid Flow
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Verified Static Density of Fluid over Flat Plate
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Verified Static Temperature over Flat Plate using Static Mach Number
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Verified Static Viscosity using Wall Temperature and Static Temperature
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3 More Static Parameters for Hypersonic Flow Calculators
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Verified Elevator Area given Hinge Moment Coefficient
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Verified Elevator Area given Stick Force
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Verified Elevator Hinge moment coefficient
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Verified Elevator Hinge Moment given Hinge Moment Coefficient
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Verified Flight Velocity for given Stick Force
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Verified Gearing Ratio
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Verified Gearing Ratio given Hinge Moment Coefficient
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Verified Hinge Moment for given Gearing Ratio
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Verified Hinge Moment for given Stick Force
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Verified Stick Deflection Angle for given Stick Force
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Verified Stick Length for given Stick Force
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12 More Stick Forces and Hinge Moments Calculators
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Verified Large Mach Number over Flat Plate using Static Temperature and Wall Temperature
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Verified Pressure Ratio for Cold-Wall Case Strong Interaction
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Verified Pressure Ratio for Cold-Wall Case Weak Interaction
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Verified Viscosity of Wall using Wall Temperature and Static Temperature
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Verified Wall Density of Fluid over Flat Plate
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3 More Supersonic Aerothermodynamics Calculators
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Verified Tail Area for given Tail Moment Coefficient
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Verified Tail Efficiency for given Pitching Moment Coefficient
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Verified Tail Lift for given Tail Pitching Moment
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Verified Tail Moment Arm for given Tail Moment Coefficient
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Verified Tail Pitching Moment Coefficient
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Verified Tail Pitching Moment Coefficient for given Tail Efficiency
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Verified Tail Pitching Moment for given Lift Coefficient
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12 More Tail Contribution Calculators
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Verified Liftoff velocity for given weight
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14 More Take Off Calculators
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Verified Mach Number
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Verified Stagnation Temperature
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17 More Thermodynamics and Governing Equations Calculators
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Verified Minimum Thrust required for given Lift Coefficient
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Verified Power required for given total drag force
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Verified Thrust for given coefficients of lift and drag
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Verified Thrust of aircraft required for given Lift-to-drag ratio
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Verified Weight of Aircraft for given Coefficients of Lift and Drag
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Verified Weight of Aircraft for given Lift-to-Drag Ratio
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13 More Thrust and Power Requirements Calculators
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Created Thrust force for given cutting force, shear angle and force along shear force
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Created Thrust force for given cutting force, shear angle and force normal to shear force
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2 More Thrust Force Calculators
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Created Average Height of Irregularities for Turbulent Flow in Pipes
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Created Discharge through Pipe given Head Loss in Turbulent Flow
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Created Head Loss due to Friction given Power Required in Turbulent Flow
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Created Power Required to Maintain Turbulent Flow
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Created Roughness Reynold Number for Turbulent Flow in Pipes
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Created Shear Stress Developed for Turbulent Flow in Pipes
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Created Shear Velocity for Turbulent Flow in Pipes
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11 More Turbulent Flow Calculators
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Verified Stream Function for Uniform Incompressible Flow
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3 More Uniform Flow Calculators
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Created Coefficient of velocity
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Created Coefficient of velocity for horizontal and vertical distance
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Created Coefficient of Velocity given Head Loss
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Created Theoretical velocity
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Created Time of Emptying Circular Horizontal Tank
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Created Time of Emptying Hemispherical Tank
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Created Time of Emptying Tank through Orifice at Bottom
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Created Velocity of liquid at C-C for Hc, Ha, and H
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Verified Aerodynamic Heating Equation for Stanton number
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Verified Coefficient of Friction using Stanton Number for Flat Plate Case
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Verified Drag per Unit Span
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Verified Prandtl Number for Flat Plate with Viscous Flow
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Verified Recovery Factor using Temperature
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Verified Skin-Friction Drag for Flat Plate in Viscous Flow
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Verified Static Density Equation using Aerodynamic Equation
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Verified Static Velocity Equation using Aerodynamic Heating Equation
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7 More Viscous Flow Calculators
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Verified Stream Function for 2-D Vortex Flow
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2 More Vortex Flow Calculators
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Verified Wall Temperature over Flat Plate using Static Mach Number
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3 More Wall Temperature Calculators
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Verified Angle of incidence of tail
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Verified Lift due to Tail only
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Verified Lift due to Wing only
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Verified Tail area for given tail efficiency
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Verified Tail Efficiency for given lift coefficients
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Verified Tail Lift Coefficient for given Pitching Moment
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Verified Tail Lift Coefficient for given Pitching Moment Coefficient
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Verified Tail Lift Coefficient of Wing-Tail Combination
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Verified Total Lift of Wing-Tail Combination
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Verified Wing Lift Coefficient of wing-tail combination
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5 More Wing Tail Contribution Calculators
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Verified Wing Area for given Moment Produced by Vertical Tail
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Verified Wing Dynamic Pressure for given Yawing Moment Coefficient
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Verified Wingspan for given Yawing Moment Coefficient
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9 More Wing Tail Interaction Calculators
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