Calculator A to Z

Calculators Created by Vinay Mishra

Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
https://www.linkedin.com/in/imvk93/
338
Formulas Created
141
Formulas Verified
99
Across Categories

List of Calculators by Vinay Mishra

Following is a combined list of all the calculators that have been created and verified by Vinay Mishra. Vinay Mishra has created 338 and verified 141 calculators across 99 different categories till date.
2 Layers (4)
Verified Heat Flow Rate through Composite Wall of 2 Layers in Series
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Verified Interface Temperature of Composite Wall of 2 Layers given Inner Surface Temperature
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Verified Length of 2nd Layer of Composite Wall in Conduction through Walls
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Verified Outer Surface Temperature of Composite Wall of 2 Layers for Conduction
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4 More 2 Layers Calculators
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3 Layers (2)
Verified Heat Flow Rate through Composite Wall of 3 Layers in Series
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Verified Outer Surface Temperature of Composite Wall of 3 Layers for Conduction
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4 More 3 Layers Calculators
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Across Shock Wave (3)
Verified Density Ratio across Normal Shock
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Created Entropy Change across Normal Shock
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Verified Pressure Ratio across Normal Shock
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2 More Across Shock Wave Calculators
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Aerodynamic Nomenclature (17)
Created Aerodynamic axial force
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Created Aerodynamic normal force
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Created Aerodynamic side force
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Created Angle of attack
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Created Normal force coefficient with aerodynamic normal force
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Created Pitching moment
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Created Pitching moment coefficient
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Created Rolling moment
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Created Rolling moment coefficient
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Created Side force coefficient
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Created Sideslip angle
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Created Velocity along pitch axis for small sideslip angle
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Created Velocity along roll axis for small angle of attack
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Created Velocity along roll axis for small sideslip angle
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Created Velocity along yaw axis for small angle of attack
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Created Yawing moment
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Created Yawing moment coefficient
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Ahead Shock Wave (3)
Verified Density ahead of Normal Shock using Normal Shock Momentum Equation
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Verified Static Pressure ahead of Normal Shock using Normal Shock Momentum Equation
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Verified Velocity ahead of Normal Shock from Normal Shock Energy Equation
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2 More Ahead Shock Wave Calculators
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Altitude Effects on Power Required and Available (6)
Created Power required at Altitude
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Created Power required at Altitude given Power at sea-level
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Created Power required at sea-level conditions
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Created Velocity at Altitude
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Created Velocity at Altitude given Velocity at Sea-Level
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Created Velocity at sea-level condition
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1 More Altitude Effects on Power Required and Available Calculators
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Approximate Results Applied to Hypersonic Vehicles (4)
Verified Adiabatic Wall Enthalpy over Flat Plate using Stanton Number
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Verified Freestream Density over Flat Plate using Stanton Number
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Verified Freestream Velocity over Flat Plate using Stanton Number
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Verified Wall Enthalpy over Flat Plate using Stanton Number
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11 More Approximate Results Applied to Hypersonic Vehicles Calculators
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Atmosphere (5)
Created Absolute altitude
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Created Geometric altitude
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Created Geometric altitude for given geopotential altitude
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Created Geopotential altitude
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Created Lapse rate
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Basic Compressible Flow (6)
Verified Critical Density
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Verified Critical Pressure
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Verified Critical Temperature
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Created Ratio of Stagnation and Static Density
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Created Ratio of Stagnation and Static Pressure
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Created Ratio of Stagnation and Static Temperature
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Basics (8)
Created Friction Coefficient
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Verified Isentropic compressibility for given density and speed of sound
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Created Mach Angle
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Created Mach Number
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Created Mayer's formula
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Created Speed of Sound
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Created Stagnation Temperature
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Verified Thermal resistance for conduction through 2 resistances in parallel
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Basics of HMT (2)
Verified Total Thermal Resistance for Conduction through Three Resistances in Series
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Verified Total Thermal Resistance for Conduction through Two Resistances in Series
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3 More Basics of HMT Calculators
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Basics of Viscous Flow (4)
Verified Buoyant Force in Falling Sphere Resistance Method
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Verified Density of Fluid in Falling Sphere Resistance Method
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Verified Diameter of Sphere in Falling Sphere Resistance Method
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Verified Drag Force in Falling Sphere Resistance Method
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15 More Basics of Viscous Flow Calculators
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Behind Shock Wave (7)
Created Characteristic Mach Number behind Shock
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Verified Density behind Normal Shock using Normal Shock Momentum Equation
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Created Mach Number behind Shock
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Verified Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
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Verified Static Pressure behind of Normal Shock using Normal Shock Momentum Equation
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Created Velocity behind Normal Shock
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Verified Velocity behind of Normal Shock from Normal Shock Energy Equation
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6 More Behind Shock Wave Calculators
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Blast-wave part 2 (2)
Verified Pressure Coefficient for Blast Wave Theory at Very High Values of Mach
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Verified Pressure Coefficient for Blunt-Nosed Plate
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4 More Blast-wave part 2 Calculators
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Bodies Connected by String and Lying on Rough Inclined Plane (6)
Created Acceleration of System given Mass of Body A
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Created Acceleration of System given Mass of Body B
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Created Frictional Force on Body A
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Created Frictional Force on Body B
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Created Tension in String given Mass of Body A
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Created Tension in String given Mass of Body B
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Bodies Connected by String and Lying on Smooth Inclined Planes (4)
Created Acceleration of System with Bodies Connected by String and Lying on Smooth Inclined Planes
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Created Angle of Inclination of Plane with Body A
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Created Angle of Inclination of Plane with Body B
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Created Tension in String if Both Bodies are Lying on Smooth Inclined Planes
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Bodies Connected by String and Passing over Smooth Pulley (3)
Created Acceleration of Bodies
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Created Mass of Body B of Smaller Mass
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Created Tension in String if Both Bodies are Freely Hanging
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Bodies Connected by String One Hanging Free Other Lying on Rough Horizontal Plane (2)
Created Acceleration of System with Bodies One Hanging Free and Other Lying on Rough Horizontal Plane
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Created Tension in String given Coefficient of Friction of Horizontal Plane
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Bodies Connected by String One Hanging Free Other Lying on Rough Inclined Plane (7)
Created Acceleration of System with Bodies One Hanging Free, Other Lying on Rough Inclined Plane
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Created Coefficient of Friction given Frictional Force
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Created Coefficient of Friction given Tension
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Created Frictional Force
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Created Inclination of Plane for given Frictional Force
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Created Mass of Body B given Frictional Force
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Created Tension in String given Coefficient of Friction of Inclined Plane
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Bodies Connected by String One Hanging Free Other Lying on Smooth Horizontal Plane (2)
Created Acceleration in System
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Created Tension in String if only One Body is Freely Suspended
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Bodies Connected by String One Hanging Free Other Lying on Smooth Inclined Plane (4)
Created Acceleration of System with Bodies One Hanging Free and Other Lying on Smooth Inclined Plane
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Created Angle of Inclination given Acceleration
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Created Angle of Inclination given Tension
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Created Tension in String when One Body is Lying on Smooth Inclined Plane
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Boundary Layer Flow (5)
Verified Average Coefficient of Drag for Drag Force
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Verified Drag Force for Average Drag Coefficient
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Verified Freestream Velocity for Local Drag Coefficient
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Verified Local Drag Coefficient for Shear Stress
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Verified Shear Stress for Local Drag Coefficient
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16 More Boundary Layer Flow Calculators
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Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions (2)
Verified Local Skin-Friction Coefficient
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Verified Stanton Number with Reynolds Number, Nusselt's Number, Stanton Number and Prandtl Number
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18 More Boundary-Layer Equations for Hypersonic Flow: Self-Similar Solutions Calculators
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Buoyancy (4)
Verified Centre of Buoyancy
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Verified Meta-centric height for time period of oscillation and radius of gyration
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Verified Radius of gyration for metacentric height and time period of oscillation
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Verified Volume of fluid displaced
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7 More Buoyancy Calculators
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Circulation (1)
Verified Circulation for Lift Force on Cylinder
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3 More Circulation Calculators
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Coefficient of Discharge (1)
Verified Coefficient of Discharge given Time of Emptying Circular Horizontal Tank
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4 More Coefficient of Discharge Calculators
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Coefficient of Velocity (1)
Verified Coefficient of Velocity given Head Loss
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2 More Coefficient of Velocity Calculators
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Coefficient's (2)
Verified Lift Coefficient for Rotating Cylinder with Circulation
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Verified Lift Coefficient for Rotating Cylinder with Tangential Speed
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3 More Coefficient's Calculators
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Compressible Flow (1)
Verified Bulk Modulus for Velocity of Sound Wave
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6 More Compressible Flow Calculators
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Conduction in Cylinder (8)
Verified Heat Flow Rate through Cylindrical Composite Wall of 2 Layers
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Verified Heat Flow Rate through Cylindrical Composite Wall of 3 Layers
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Verified Heat Flow Rate through Cylindrical Wall
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Verified Inner Surface Temperature of Cylindrical Wall in Conduction
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Verified Outer Surface Temperature of Cylindrical Composite Wall of 2 Layers
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Verified Outer Surface Temperature of Cylindrical Wall given Heat Flow Rate
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Verified Thermal Conductivity of Cylindrical Wall given Temperature Difference
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Verified Thermal Resistance for Radial Heat Conduction in Cylinders
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6 More Conduction in Cylinder Calculators
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Conduction in Plane Wall (4)
Verified Area of Plane Wall Required for Given Temperature Difference
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Verified Outer Surface Temperature of Wall in Conduction through Wall
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Verified Thermal Conductivity of Material Required to Maintain Given Temperature Difference
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Verified Thickness of Plane Wall for Conduction through Wall
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4 More Conduction in Plane Wall Calculators
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Contribution of Aircraft Components- Part 1 (15)
Created Moment produced by vertical tail for given lift curve slope
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Created Moment produced by vertical tail for given side force
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Created Sideslip angle for Aircraft
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Created Sideslip angle for given moment produced by vertical tail
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Created Sidewash angle
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Created Vertical tail angle of attack
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Created Vertical tail angle of attack for given vertical tail side force
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Created Vertical tail area for given vertical tail side force
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Created Vertical tail dynamic pressure for given vertical tail side force
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Created Vertical tail lift curve slope
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Created Vertical tail lift curve slope for given moment
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Created Vertical tail moment arm for given lift curve slope
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Created Vertical tail moment arm for given side force
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Created Vertical tail Side force
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Created Vertical tail side force for given moment
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Contribution of Aircraft Components- Part 2 (14)
Created Dynamic pressure at vertical tail for given yawing moment coefficient
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Created Moment produced by vertical tail for given moment coefficient
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Created Sideslip angle for given yawing moment coefficient
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Created Sidewash angle for given moment produced by vertical tail
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Created Sidewash Angle given Yawing Moment Coefficient using Wingspan
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Created Vertical tail area for given moment
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Created Vertical tail area for given yawing moment coefficient
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Created Vertical tail dynamic pressure for given moment
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Created Vertical tail lift curve slope for given yawing moment coefficient
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Created Wing area for given moment produced by vertical tail
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Created Wing dynamic pressure for given yawing moment coefficient
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Created Wingspan for given yawing moment coefficient
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Created Yawing moment coefficient for given vertical tail lift curve slope
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Created Yawing Moment Coefficient using Wingspan
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Contribution of Aircraft Components- Part 3 (15)
Created Dynamic pressure at vertical tail for given vertical tail efficiency
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Created Dynamic pressure at wing for given vertical tail efficiency
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Created Dynamic pressure at wing for given yawing moment coefficient
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Created Vertical tail area for given vertical tail volume ratio
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Created Vertical tail efficiency
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Created Vertical tail efficiency for given yawing moment coefficient
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Created Vertical tail lift curve slope for given yawing moment coefficient and Vertical Tail Efficiency
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Created Vertical tail moment arm for given vertical tail volume ratio
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Created Vertical tail volume ratio
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Created Vertical tail volume ratio for given yawing moment coefficient
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Created Wing area for given vertical tail volume ratio
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Created Wing area for given yawing moment coefficient
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Created Wingspan for given vertical tail volume ratio
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Created Wingspan for yawing moment coefficient given sideslip angle and sidewash angle
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Created Yawing moment coefficient for given vertical tail volume ratio
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Contribution of Aircraft Components- Part 4 (2)
Created Sideslip angle for yawing moment coefficient given vertical tail volume ratio
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Created Sidewash angle for given yawing moment coefficient
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Cylindrical Blast Wave (1)
Verified Modified Energy for Cylindrical Blast Wave
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6 More Cylindrical Blast Wave Calculators
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Discharge (3)
Verified Discharge through fully sub-merged orifice
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Verified Discharge through large rectangular orifice
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Verified Discharge through partially sub-merged orifice
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3 More Discharge Calculators
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Discharge (4)
Verified Discharge over Broad-Crested Weir
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Verified Discharge over Rectangle Notch or Weir
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Verified Discharge over Rectangle Weir for Bazin's formula with Velocity of Approach
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Verified Discharge over Rectangle Weir with Two End Contractions
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9 More Discharge Calculators
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Drag during Level Unaccelerated Flight (7)
Created Coefficient of Drag for given thrust and weight
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Created Coefficient of Drag for given thrust-to-weight ratio
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Created Drag for Level and Unaccelerated Flight at Negligible Thrust Angle
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Created Lift-induced drag coefficient for given required thrust
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Created Zero-lift drag coefficient at minimum required thrust
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Created Zero-lift drag coefficient for given lift coefficient
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Created Zero-lift drag coefficient for given required thrust
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Drag Polar (4)
Created Coefficient of Drag due to lift
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Created Drag Coefficient for given parasite drag coefficient
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Created Drag Coefficient for given zero-lift drag coefficient
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Created Parasite Drag Coefficient at zero lift
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Elevator and Stick Deflection Angles (4)
Created Elevator deflection angle for given gearing ratio
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Created Elevator deflection angle for given stick force
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Created Stick deflection angle for given gearing ratio
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Created Stick deflection angle for given stick force
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Equations of Motion (11)
Created Centrifugal Force in Accelerated Flight
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Created Drag for Level and Unaccelerated Flight
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Created Drag in Accelerated Flight
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Created Lift for Unaccelerated Flight
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Created Lift in Accelerated Flight
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Created Thrust angle for unaccelerated flight for given drag
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Created Thrust Angle for Unaccelerated Flight for given Lift
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Created Thrust for Level and Unaccelerated Flight
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Created Thrust in Accelerated Flight
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Created Velocity in accelerated flight
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Created Weight of aircraft in level, unaccelerated flight
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Expansion Fan (3)
Verified Pressure behind Expansion Fan
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Verified Rearward Mach Angle of Expansion Fan
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Verified Temperature behind Expansion Fan
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3 More Expansion Fan Calculators
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Flight Envelope (15)
Created Lift Coefficient for given turn radius
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Created Lift Coefficient for given turn rate
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Created Lift Coefficient for given wing loading and turn radius
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Created Load factor for given turn radius for high-performance fighter aircraft
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Created Load factor for given turn rate for high-performance fighter aircraft
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Created Radius of turn for given lift coefficient
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Created Radius of turn for given wing loading
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Created Turn radius for high load factor
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Created Turn rate for given lift coefficient
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Created Turn rate for given wing loading
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Created Turn rate for high load factor
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Created Velocity for given turn rate for high load factor
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Created Velocity given Turn Radius for High Load Factor
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Created Wing loading for given turn radius
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Created Wing loading for given turn rate
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1 More Flight Envelope Calculators
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Gearing Ratio (4)
Created Control stick length for given gearing ratio
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Created Gearing ratio
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Created Gearing ratio for given hinge moment coefficient
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Created Gearing ratio for given stick force
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Gibbs Phase Rule (4)
Created Degree of Freedom
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Created Number of Components
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Created Number of Phases
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Created Total Number of Variables in System
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Gliding Flight (5)
Created Drag for given glide angle
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Created Glide angle
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Created Glide angle for given lift-to-drag ratio
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Created Lift force for given glide angle
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Created Lift-to-drag ratio for given glide angle
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Hinge Moment (3)
Created Hinge moment coefficient for given stick force
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Created Hinge moment for given gearing ratio
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Created Hinge moment for given stick force
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Hypersonic Equivalence Principle and Blast-Wave Theory (1)
Verified Coefficient of Drag Equation using Energy Released from Blast Wave
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8 More Hypersonic Equivalence Principle and Blast-Wave Theory Calculators
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Hypersonic Transition (3)
Verified Reynolds Number Equation using Boundary-Layer Momentum Thickness
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Verified Reynolds Number Equation using Local Mach Number
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Verified Thermal Conductivity of Transition Flow
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13 More Hypersonic Transition Calculators
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Ideal flow or Potential flow (8)
Verified Radial velocity at any radius
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Verified Radius at any point considering radial velocity
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Verified Stream function at point
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Verified Stream Function at Point in Combined Flow
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Verified Stream function in sink flow for angle
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Verified Strength of doublet for stream function
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Verified Strength of source for radial velocity and at any radius
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Verified Uniform flow velocity for stream function at point in combined flow
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6 More Ideal flow or Potential flow Calculators
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Incompressible flow over airfoil (1)
Verified Lift Coefficient for Symmetrical Airfoil by Thin Airfoil Theory
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7 More Incompressible flow over airfoil Calculators
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Introduction (7)
Verified Circulation by Kutta-Joukowski Theorem
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Verified Height Difference of Manometric Fluid for given Pressure Difference
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Verified Location of Stagnation Point Outside Cylinder for Lifting Flow
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Verified Radius of Cylinder for Non-Lifting Flow
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Verified Source Strength for 2-D Incompressible Source Flow
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Verified Stagnation Streamline Equation for Flow over Semi-Infinite Body
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Verified Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity
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9 More Introduction Calculators
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Laminar Boundary Layer at Stagnation point on Blunt body (2)
Verified Reynolds Analogy Factor in Finite Deference Method
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Verified Reynolds Analogy for Stanton Number in Finite Difference Method
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5 More Laminar Boundary Layer at Stagnation point on Blunt body Calculators
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Landing Performance (4)
Created Landing ground roll distance
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Created Stall velocity for given touchdown velocity
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Created Touchdown velocity
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Created Touchdown velocity for given stall velocity
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Length of Weir (2)
Verified Length of Weir Considering Bazin's formula with Velocity of Approach
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Verified Length of Weir for Discharge over Broad-Crested Weir
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6 More Length of Weir Calculators
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Lift Force on Body (2)
Verified Length of Cylinder for Lift Force on Cylinder
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Verified Lift Force on Cylinder for Circulation
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5 More Lift Force on Body Calculators
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Lift to Drag (3)
Created Lift-to-drag ratio for given required thrust of aircraft
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Created Thrust of aircraft required for given Lift-to-drag ratio
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Created Weight of aircraft for given Lift-to-drag ratio
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Longitudinal Control of Elevator Hinge Moment (5)
Created Elevator area for given hinge moment coefficient
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Created Elevator chord length for given hinge moment coefficient
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Created Elevator Hinge moment coefficient
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Created Elevator Hinge moment for given hinge moment coefficient
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Created Flight velocity for given elevator hinge moment coefficient
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Loss of Head (2)
Verified Loss of Head due to Bend in Pipe
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Verified Loss of head due to sudden enlargement at any particular section of pipe
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6 More Loss of Head Calculators
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Maneuvering Flight (12)
Created Load Factor given Pull-down Maneuver Radius
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Created Load Factor given Pull-down Maneuver Rate
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Created Load Factor given Pull-UP Maneuver Radius
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Created Load Factor given Pull-Up Maneuver Rate
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Created Pull-down maneuver radius
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Created Pull-down maneuver rate
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Created Pull-up maneuver radius
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Created Pull-up maneuver rate
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Created Velocity for given pull-down maneuver rate
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Created Velocity for given pull-up maneuver radius
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Created Velocity for given pull-up maneuver rate
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Created Velocity given Pull-down Maneuver Radius
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1 More Maneuvering Flight Calculators
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Merchant Force Circle (Mechanics of Orthogonal metal cutting) (5)
Created Cutting Shear Force given Uncut Chip Thickness and Shear Angle
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Created Shear angle for given area of shear plane, width of cut and uncut chip thickness
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Created Shear force acting on shear plane for given shear stress and area of shear plane
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Created Uncut chip thickness for given width of cut, shear angle and area of shear plane
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Created Width of cut for given shear angle, uncut chip thickness and area of shear plane
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17 More Merchant Force Circle (Mechanics of Orthogonal metal cutting) Calculators
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Metal Cutting and Tools (4)
Created Back Rake Angle
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Created Inclination Angle
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Created Orthogonal Rake Angle
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Created Side Rake Angle
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2 More Metal Cutting and Tools Calculators
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Modern design-oriented code (1)
Verified Radiative Heat Transfer to Surface Stemming from Thermal Radiation
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1 More Modern design-oriented code Calculators
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Normal Shock Waves (4)
Created Characteristic Mach Number
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Created Prandtl Condition
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Created Relation between Characteristic Mach Number and Mach Number
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Created Shock Strength
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4 More Normal Shock Waves Calculators
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Notches and Weirs (2)
Verified Head of Liquid at Crest
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Verified Length of Section for Discharge over Rectangle Notch or Weir
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4 More Notches and Weirs Calculators
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Oblique Shock (2)
Created Component of Downstream Mach Normal to Oblique Shock
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Created Component of Upstream Mach Normal to Oblique Shock
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7 More Oblique Shock Calculators
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Oblique Shock and Expansion Waves (3)
Created Flow Deflection Angle
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Verified Prandtl Meyer Function
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Verified Prandtl Meyer Function at Upstream Mach Number
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1 More Oblique Shock and Expansion Waves Calculators
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Oblique Shock Relation (2)
Created Dynamic Pressure for given Specific Heat Ratio and Mach Number
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Verified Velocity of Sound using Dynamic Pressure and Density
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13 More Oblique Shock Relation Calculators
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Orifices and Mouthpieces (3)
Verified Head of liquid for head loss and coefficient of velocity
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Verified Loss of head due to fluid resistance
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Verified Theoretical velocity
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13 More Orifices and Mouthpieces Calculators
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Parameters (2)
Verified Axial Force Coefficient
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Verified Normal Force Coefficient
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18 More Parameters Calculators
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Power Available and Maximum Velocity (3)
Created Power available for reciprocating engine-propeller combination
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Created Propeller efficiency for reciprocating engine-propeller combination
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Created Shaft brake power for reciprocating engine-propeller combination
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Power Required for Level Unaccelerated Flight (10)
Created Coefficient of Drag due to lift for minimum power required
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Created Freestream velocity for given required power
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Created Freestream Velocity for given total drag force
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Created Power required for given aerodynamic coefficients
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Created Power required for given required thrust of aircraft
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Created Power required for given total drag force
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Created Thrust of aircraft required for given required power
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Created Total drag force for given required power
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Created Weight of aircraft for given required power
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Created Zero-lift drag coefficient for minimum power required
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Pressure (4)
Verified Pressure at Downstream Point on Streamline by Bernoulli's Equation
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Verified Pressure Difference in Low-Speed Wind Tunnel for given Test Section Velocity
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Verified Surface Pressure Coefficient for Lifting Flow over Circular Cylinder
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Verified Surface Pressure on Body using Pressure Coefficient
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9 More Pressure Calculators
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Radial Velocity (1)
Verified Radial Velocity for Lifting Flow over Circular Cylinder
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2 More Radial Velocity Calculators
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Range and Endurance of Jet Airplane (7)
Created Endurance for given Lift-to-Drag ratio of Jet Airplane
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Created Endurance of Jet Airplane
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Created Lift-to-Drag ratio for given Endurance of Jet Airplane
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Created Range of Jet Airplane
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Created Thrust-Specific Fuel Consumption for given Endurance and Lift-to-Drag ratio of Jet Airplane
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Created Thrust-Specific Fuel Consumption for given Endurance of Jet Airplane
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Created Thrust-Specific Fuel Consumption for given Range of Jet Airplane
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1 More Range and Endurance of Jet Airplane Calculators
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Range and Endurance of Propeller-Driven Airplane (10)
Created Endurance of Propeller-Driven Airplane
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Created Lift-to-Drag ratio for given Range of Propeller-Driven Airplane
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Created Propeller Efficiency for given Endurance of Propeller-Driven Airplane
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Created Propeller Efficiency for given Range and lift-to-drag ratio of Propeller-Driven Airplane
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Created Propeller Efficiency for given Range of Propeller-Driven Airplane
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Created Range of Propeller-Driven Airplane
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Created Range of Propeller-Driven Airplane for given lift-to-drag ratio
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Created Specific Fuel Consumption for given Endurance of Propeller-Driven Airplane
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Created Specific Fuel Consumption for given Range and lift-to-drag ratio of Propeller-Driven Airplane
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Created Specific Fuel Consumption for given Range of Propeller-Driven Airplane
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Rate of Climb (10)
Created Excess power
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Created Excess power for given rate of climb
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Created Flight path angle at given rate of climb
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Created Rate of Climb
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Created Rate of Climb for given excess power
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Created Thrust available for given excess power
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Created Total Drag for given excess power
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Created Velocity of aircraft at given rate of climb
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Created Velocity of aircraft for given excess power
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Created Weight of aircraft for given excess power
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Reference Temperature Method (3)
Verified Local Turbulent Skin-Friction Coefficient for Incompressible Flow
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Verified Reynolds Number for Chord Length using Overall Skin-Friction Drag Coefficient
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Verified Turbulent Flat-Plate Skin-Friction Coefficient
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12 More Reference Temperature Method Calculators
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Roll Stability (5)
Created Aircraft forward velocity for given normal component of side velocity
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Created Aircraft sideslip velocity for given dihedral angle
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Created Dihedral angle for given sideslip velocity
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Created Normal component of aircraft side velocity for given dihedral angle
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Created Normal component of aircraft side velocity for given forward velocity
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Stagnation Points (1)
Verified Radius of Cylinder for Lift Coefficient in Rotating Cylinder with Circulation
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3 More Stagnation Points Calculators
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Stick Forces (7)
Created Elevator area for given stick force
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Created Elevator chord length for given stick force
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Created Elevator Stick Force
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Created Elevator Stick force for given gearing ratio
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Created Elevator stick force for given hinge moment coefficient
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Created Flight velocity for given stick force
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Created Stick length for given stick force
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Stream Function (2)
Verified Stream Function for 2-D Incompressible Source Flow
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Verified Stream Function for Non-Lifting Flow over Circular Cylinder
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7 More Stream Function Calculators
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Tail Contribution (21)
Created Angle of Attack at Tail
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Created Angle of attack of wing
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Created Angle of incidence of tail
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Created Angle of incidence of wing
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Created Downwash angle
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Created Lift due to tail only
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Created Lift due to wing only
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Created Mean aerodynamic chord for given tail pitching moment coefficient
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Created Pitching moment due to tail
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Created Tail area for given tail efficiency
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Created Tail Efficiency for given lift coefficients
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Created Tail lift coefficient for given pitching moment
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Created Tail Lift Coefficient of wing-tail combination
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Created Tail lift for given tail pitching moment
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Created Tail Pitching moment coefficient
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Created Tail Pitching moment for given lift coefficient
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Created Tail Pitching moment for given moment coefficient
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Created Total Lift Coefficient of wing-tail combination
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Created Total Lift of wing-tail combination
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Created Vertical tail moment arm for given yawing moment coefficient
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Created Wing Lift Coefficient of wing-tail combination
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Tail Contribution Contd (14)
Created Horizontal tail area for given tail volume ratio
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Created Horizontal tail volume ratio
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Created Horizontal tail volume ratio for given pitching moment coefficient
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Created Tail area for given tail moment coefficient
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Created Tail Efficiency for given pitching moment coefficient
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Created Tail Efficiency for given tail volume ratio
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Created Tail lift coefficient for given pitching moment coefficient
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Created Tail lift coefficient for given tail volume ratio
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Created Tail moment arm for given horizontal tail volume ratio
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Created Tail moment arm for given tail moment coefficient
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Created Tail Pitching moment coefficient for given tail efficiency
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Created Tail Pitching moment coefficient for given tail volume ratio
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Created Wing Mean aerodynamic chord for given horizontal tail volume ratio
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Created Wing Reference area for given horizontal tail volume ratio
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Takeoff Performance (14)
Created Coefficient of rolling friction during ground roll
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Created Drag during ground effect
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Created Ground effect factor
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Created Lift acting on aircraft during ground roll
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Created Liftoff distance
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Created Liftoff velocity for given stall velocity
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Created Liftoff velocity for given weight
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Created Maximum Lift coefficient for given liftoff velocity
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Created Maximum Lift coefficient for given stall velocity
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Created Resistance force during ground roll
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Created Stall velocity for given liftoff velocity
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Created Stall velocity for given weight
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Created Thrust for given liftoff distance
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Created Weight of aircraft during ground roll
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Thrust Required for Level Unaccelerated Flight (12)
Created Coefficient of Lift for given thrust and weight
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Created Coefficient of Lift for given thrust-to-weight ratio
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Created Lift coefficient for given minimum required thrust
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Created Lift for Level and Unaccelerated Flight at Negligible Thrust Angle
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Created Minimum Thrust of aircraft required
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Created Minimum Thrust required for given lift coefficient
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Created Minimum Thrust required for given weight
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Created Thrust for given coefficients of lift and drag
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Created Thrust of aircraft required for level, unaccelerated flight
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Created Thrust-to-weight ratio
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Created Weight of aircraft for given coefficients of lift and drag
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Created Weight of aircraft for level, unaccelerated flight at negligible thrust angle
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Time of Emptying (1)
Verified Time of Emptying Circular Horizontal Tank
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2 More Time of Emptying Calculators
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Turbulent Flow (2)
Verified Discharge through Pipe given Head Loss in Turbulent Flow
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Verified Head Loss due to Friction given Power Required in Turbulent Flow
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16 More Turbulent Flow Calculators
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Turning Flight (12)
Created Bank angle during level turn
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Created Lift during level turn
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Created Lift for given load factor
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Created Load factor given Lift Force and Weight of Aircraft
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Created Load Factor given Turn Radius
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Created Load Factor given Turn Rate
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Created Turn radius
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Created Turn rate
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Created Velocity for given turn radius
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Created Velocity for given turn rate
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Created Weight for given load factor
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Created Weight of aircraft during level turn
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Valves (2)
Verified Intensity of pressure wave produced for gradual closure of valves
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Verified Time required to close Valve for Gradual Closure of Valves
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2 More Valves Calculators
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Velocity (1)
Verified Velocity of Sphere in Falling Sphere Resistance Method
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4 More Velocity Calculators
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Velocity (3)
Verified Freestream Velocity for Lift Coefficient in Rotating Cylinder with Circulation
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Verified Freestream velocity for lift coefficient with tangential speed
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Verified Tangential Velocity of Cylinder with Lift Coefficient
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3 More Velocity Calculators
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Velocity of Flow (2)
Verified Velocity at section 1-1 for sudden enlargement
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Verified Velocity at section 2-2 for sudden enlargement
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7 More Velocity of Flow Calculators
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Velocity of Sound Wave (1)
Verified Velocity of Sound Wave given Bulk Modulus
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5 More Velocity of Sound Wave Calculators
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Velocity Potential (2)
Verified Velocity Potential for 2-D Vortex Flow
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Verified Velocity Potential for Uniform Incompressible Flow
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3 More Velocity Potential Calculators
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Viscosity of Fluid (1)
Verified Viscosity of Fluid or Oil in Falling Sphere Resistance Method
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4 More Viscosity of Fluid Calculators
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Viscous Flow (3)
Verified Recovery Factor Calculation using Prandtl Number
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Verified Recovery Factor for Flat Plate with Viscous Flow
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Verified Skin-Friction Drag Coefficient
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12 More Viscous Flow Calculators
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Wall Temperature (1)
Verified Wall Temperature over Flat Plate under Viscous, Very High Mach Flow
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3 More Wall Temperature Calculators
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