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Calculators Created by Shikha Maurya
Shikha Maurya
Indian Institute of Technology
(IIT)
,
Bombay
https://www.linkedin.com/in/shikha-maurya-eager-to-learn/
108
Formulas Created
170
Formulas Verified
75
Across Categories
List of Calculators by Shikha Maurya
Following is a combined list of all the calculators that have been created and verified by Shikha Maurya. Shikha Maurya has created 108 and verified 170 calculators across 75 different categories till date.
Aero Thermal Dynamics
(3)
Verified
Non Dimensional Internal Energy Parameter using Wall-to-Freestream Temperature Ratio
Go
Verified
Non Dimensional Static Enthalpy
Go
Verified
Stanton Equation using Overall Skin Friction Coefficient for Incompressible Flow
Go
13 More Aero Thermal Dynamics Calculators
Go
Aerodynamic Measurements and Wind Tunnel Testing
(10)
Created
Airspeed Measurement by Pitot Tube
Go
Created
Airspeed Measurement by Venturi
Go
Created
Dynamic Pressure in Incompressible Flow
Go
Created
Height Difference of Manometric Fluid for given Pressure Difference
Go
Created
Surface Pressure on Body using Pressure Coefficient
Go
Created
Test Section Velocity by Manometric Height for Wind Tunnel
Go
Created
Total Pressure in Incompressible Flow
Go
Created
Wind Tunnel Pressure Difference by Manometer
Go
Created
Wind Tunnel Pressure Difference with Test Speed
Go
Created
Wind Tunnel Test Section Velocity
Go
Aerodynamic Parameters
(1)
Verified
Yawing Moment Coefficient using Wingspan
Go
10 More Aerodynamic Parameters Calculators
Go
Aircraft Dynamics Nomenclature
(8)
Verified
Aerodynamic Axial Force
Go
Verified
Aerodynamic Normal Force
Go
Verified
Aerodynamic Side Force
Go
Verified
Angle of attack
Go
Verified
Pitching moment
Go
Verified
Pitching moment coefficient
Go
Verified
Side force coefficient
Go
Verified
Sideslip angle
Go
10 More Aircraft Dynamics Nomenclature Calculators
Go
Atmosphere and Gas Properties
(5)
Verified
Absolute altitude
Go
Verified
Geometric altitude
Go
Verified
Geometric altitude for given geopotential altitude
Go
Verified
Geopotential altitude
Go
Verified
Lapse rate
Go
9 More Atmosphere and Gas Properties Calculators
Go
Bending Stresses
(1)
Verified
Section Modulus of Steel Beam given Stress in Steel for Unshored Members
Go
9 More Bending Stresses Calculators
Go
Bernoulli's Equation and Pressure Concepts
(6)
Created
Pressure at Downstream Point by Bernoulli's Equation
Go
Created
Pressure at Upstream Point by Bernoulli's Equation
Go
Created
Pressure Coefficient
Go
Created
Pressure Coefficient using Velocity Ratio
Go
Created
Static Pressure in Incompressible Flow
Go
Created
Velocity at Point on Airfoil for given Pressure Coefficient and Free-Stream Velocity
Go
Blast Wave Part Theory
(3)
Verified
Pressure Coefficient Combined with Blast Wave for Shuttle
Go
Verified
Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack
Go
Verified
Pressure Coefficient for Blunt-Nosed Cylinder
Go
3 More Blast Wave Part Theory Calculators
Go
Body Lying on Rough Horizontal Plane
(1)
Verified
Acceleration of System with Bodies One Hanging Free and Other Lying on Rough Horizontal Plane
Go
1 More Body Lying on Rough Horizontal Plane Calculators
Go
Body Lying on Smooth Horizontal Plane
(2)
Verified
Acceleration in System
Go
Verified
Tension in String if only One Body is Freely Suspended
Go
Body Passing Over Smooth Pulley
(3)
Verified
Acceleration of Bodies
Go
Verified
Mass of Body B of Smaller Mass
Go
Verified
Tension in String if Both Bodies are Freely Hanging
Go
Boundary Layer Flow
(4)
Verified
Drag Force on Plate
Go
Verified
Reynold Number for Drag Force on Plate
Go
Verified
Viscosity of Liquid for Drag Force on Plate
Go
Verified
Width of Plate for Drag Force on Plate
Go
17 More Boundary Layer Flow Calculators
Go
Climbing Flight
(2)
Verified
Excess power
Go
Verified
Total Drag for given Excess Power
Go
14 More Climbing Flight Calculators
Go
Compressible Flow Parameters
(3)
Verified
Mach Angle for Compressible Fluid Flow
Go
Verified
Velocity of Projectile of Mach Cone in Compressible Fluid Flow
Go
Verified
Velocity of Sound Wave considering Mach Angle in Compressible Fluid Flow
Go
7 More Compressible Flow Parameters Calculators
Go
Compression Waves
(2)
Verified
Density before Shock Formation for Compression Wave
Go
Verified
Temperature Ratio for Unsteady Compression Waves
Go
1 More Compression Waves Calculators
Go
Cutting Force
(3)
Created
Cutting force for given force along shear force, shear, friction and normal rake angles
Go
Created
Cutting force for given resultant force in merchant circle, friction angle and normal rake angle
Go
Created
Cutting force for shear stress, width of cut, uncut chip thickness, friction, rake and shear angles
Go
3 More Cutting Force Calculators
Go
Cylindrical Blast Wave
(2)
Verified
Modified Pressure Equation for Cylindrical Blast Wave
Go
Verified
Pressure Ratio for Blunt Slab Blast Wave
Go
6 More Cylindrical Blast Wave Calculators
Go
Dimensionless Quantities
(1)
Verified
Reynolds Number for given Nusselt's Number, Stanton Number and Prandtl Number
Go
3 More Dimensionless Quantities Calculators
Go
Dimensions and Geometry
(4)
Verified
Length for Difference of Pressure in Viscous Flow between Two Parallel Plates
Go
Verified
Length for Pressure Head Loss in Viscous Flow between Two Parallel Plates
Go
Verified
Length of Tube in Capillary Tube Method
Go
Verified
Radius of Capillary Tube
Go
15 More Dimensions and Geometry Calculators
Go
Discharge
(4)
Verified
Discharge over Rectangle Weir Considering Bazin's formula
Go
Verified
Discharge over Rectangle Weir Considering Francis's formula
Go
Verified
Discharge with Velocity of Approach
Go
Verified
Discharge without Velocity of Approach
Go
13 More Discharge Calculators
Go
Doublet Flow
(2)
Created
Stream Function for 2-D Doublet Flow
Go
Created
Velocity Potential for 2-D Doublet Flow
Go
Downstream Shock Waves
(10)
Created
Density behind Normal Shock given Upstream Density and Mach Number
Go
Created
Density behind Normal Shock using Normal Shock Momentum Equation
Go
Created
Enthalpy behind Normal Shock from Normal Shock Energy Equation
Go
Created
Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
Go
Created
Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
Go
Created
Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
Go
Created
Static Pressure behind Normal Shock using Normal Shock Momentum Equation
Go
Created
Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
Go
Created
Velocity behind Normal Shock by Normal Shock Momentum Equation
Go
Created
Velocity behind Normal Shock from Normal Shock Energy Equation
Go
5 More Downstream Shock Waves Calculators
Go
Drag and Forces
(3)
Verified
Area of body for Lift Force in body moving on Fluid
Go
Verified
Pressure Drag from Total Drag Force on Sphere
Go
Verified
Skin Friction Drag from Total Drag Force on Sphere
Go
8 More Drag and Forces Calculators
Go
Expansion Waves
(2)
Verified
New Pressure after Shock Formation, Subtracted to Velocity for Expansion Wave
Go
Verified
Pressure Ratio for Unsteady Waves with Subtracted Induced Mass Motion for Expansion Waves
Go
3 More Expansion Waves Calculators
Go
Expansion Waves
(9)
Created
Flow Deflection Angle using Prandtl Meyer Function
Go
Created
Forward Mach Angle of Expansion Fan
Go
Created
Prandtl Meyer Function
Go
Created
Prandtl Meyer Function at Upstream Mach Number
Go
Created
Pressure behind Expansion Fan
Go
Created
Pressure Ratio across Expansion Fan
Go
Created
Rearward Mach Angle of Expansion Fan
Go
Created
Temperature behind Expansion Fan
Go
Created
Temperature Ratio across Expansion Fan
Go
1 More Expansion Waves Calculators
Go
Flow Analysis
(4)
Verified
Difference of Pressure for Viscous Flow between Two Parallel Plates
Go
Verified
Loss of Pressure Head for Viscous Flow between Two Parallel Plates
Go
Verified
Power Absorbed in Overcoming Viscous Resistance in Journal Bearing
Go
Verified
Viscosity of Fluid or Oil for Capillary Tube Method
Go
9 More Flow Analysis Calculators
Go
Flow over Airfoils
(8)
Created
Boundary Layer Thickness for Laminar Flow
Go
Created
Boundary Layer Thickness for Turbulent Flow
Go
Created
Center of Pressure Location for Cambered Airfoil
Go
Created
Lift Coefficient for Cambered Airfoil
Go
Created
Lift Coefficient for Symmetrical Airfoil by Thin Airfoil Theory
Go
Created
Moment Coefficient about Leading-Edge for Symmetrical Airfoil by Thin Airfoil Theory
Go
Created
Skin Friction Drag Coefficient for Flat Plate in Laminar Flow
Go
Created
Skin Friction Drag Coefficient for Flat Plate in Turbulent Flow
Go
Flow Regime
(4)
Verified
Discharge in Equivalent Pipe
Go
Verified
Velocity of Flow at Outlet of Nozzle
Go
Verified
Velocity of Flow at outlet of Nozzle for Efficiency and Head
Go
Verified
Velocity of fluid in pipe for head loss at entrance of pipe
Go
13 More Flow Regime Calculators
Go
Fluid Flow and Resistance
(6)
Verified
Discharge in Capillary Tube Method
Go
Verified
Rotational Speed considering Power Absorbed and Torque in Journal Bearing
Go
Verified
Shear Force for Torque and Diameter of Shaft in Journal Bearing
Go
Verified
Shear Stress in Fluid or Oil of Journal Bearing
Go
Verified
Torque Required Considering Power Absorbed in Journal Bearing
Go
Verified
Torque Required to Overcome Shear Force in Journal Bearing
Go
15 More Fluid Flow and Resistance Calculators
Go
Force Along Shear
(1)
Created
Force along shear force for given R of merchant circle, shear, friction, and normal rake angles
Go
2 More Force Along Shear Calculators
Go
Force Normal to Shear
(1)
Created
Shear angle for given Resultant force, force along shear force, friction, and normal rake angles
Go
3 More Force Normal to Shear Calculators
Go
Forces and Friction
(1)
Created
Friction angle for given R of merchant circle, force along shear, shear, and normal rake angle
Go
5 More Forces and Friction Calculators
Go
Geometric DImension
(4)
Verified
Length of Weir Considering Bazin's formula without Velocity of Approach
Go
Verified
Length of Weir Considering Francis's formula
Go
Verified
Length of Weir or Notch for Velocity of Approach
Go
Verified
Length of Weir or Notch without Velocity of Approach
Go
6 More Geometric DImension Calculators
Go
Geometric Property
(6)
Verified
Area of Nozzle at Outlet for Maximum Power Transmission through Nozzle
Go
Verified
Area of Pipe for Maximum Power Transmission through Nozzle
Go
Verified
Diameter of Equivalent Pipe
Go
Verified
Diameter of nozzle for maximum power transmission through nozzle
Go
Verified
Length of Equivalent Pipe
Go
Verified
Length of pipe for maximum power transmission through nozzle
Go
1 More Geometric Property Calculators
Go
Geometry and Dimensions
(2)
Created
Uncut chip thickness given cutting force, shear stress, cut, friction, normal rake and shear angles
Go
Created
Width of cut given cutting force, shear stress, uncut chip, friction, normal rake and shear angles
Go
6 More Geometry and Dimensions Calculators
Go
Governing Equations and Sound Wave
(4)
Created
Critical Density
Go
Created
Critical Pressure
Go
Created
Critical Temperature
Go
Created
Isentropic Compressibility for given Density and Speed of Sound
Go
14 More Governing Equations and Sound Wave Calculators
Go
High Load Factor Maneuver
(5)
Verified
Lift Coefficient for given Turn Rate
Go
Verified
Load factor for given turn rate for high-performance fighter aircraft
Go
Verified
Radius of Turn for given Lift Coefficient
Go
Verified
Radius of Turn for given Wing Loading
Go
Verified
Turn Rate for given Wing Loading
Go
12 More High Load Factor Maneuver Calculators
Go
Hypersonic Flight Paths Velocity of Altitude Map
(1)
Verified
Blunt-Nosed Radial Coordinate Flat Plate (First Approximation)
Go
8 More Hypersonic Flight Paths Velocity of Altitude Map Calculators
Go
Hypersonic Flow Parameters
(1)
Verified
Skin Friction Coefficient for Incompressible Flow
Go
6 More Hypersonic Flow Parameters Calculators
Go
Incompressible Flow Characteristics
(1)
Verified
Distance of stagnation point S from source in flow past half body
Go
22 More Incompressible Flow Characteristics Calculators
Go
Kinematics of Flow
(2)
Verified
Coefficient of pitot-tube for velocity at any point
Go
Verified
Resultant bend force along x and y direction
Go
15 More Kinematics of Flow Calculators
Go
Kutta Joukowski Lift Theorem
(4)
Created
Circulation by Kutta-Joukowski Theorem
Go
Created
Freestream Density by Kutta-Joukowski Theorem
Go
Created
Freestream Velocity by Kutta-Joukowski Theorem
Go
Created
Lift Per Unit Span by Kutta-Joukowski Theorem
Go
Landing
(1)
Verified
Stall velocity for given touchdown velocity
Go
4 More Landing Calculators
Go
Lift and Circulation
(6)
Verified
Angle of Attack for Circulation developed on Airfoil
Go
Verified
Chord Length for Circulation developed on Airfoil
Go
Verified
Circulation developed on Airfoil
Go
Verified
Lift coefficient for lift force in body moving on fluid
Go
Verified
Lift Force for body moving in Fluid of Certain Density
Go
Verified
Velocity of Airfoil for Circulation developed on Airfoil
Go
10 More Lift and Circulation Calculators
Go
Lifting Flow over Cylinder
(6)
Created
2-D Lift Coefficient for Cylinder
Go
Created
Location of Stagnation Point Outside Cylinder for Lifting Flow
Go
Created
Radial Velocity for Lifting Flow over Circular Cylinder
Go
Created
Stream Function for Lifting Flow over Circular Cylinder
Go
Created
Surface Pressure Coefficient for Lifting Flow over Circular Cylinder
Go
Created
Tangential Velocity for Lifting Flow over Circular Cylinder
Go
4 More Lifting Flow over Cylinder Calculators
Go
Local Heat Transfer for Hypersonic Flow
(3)
Verified
Adiabatic Wall Enthalpy using Stanton Number
Go
Verified
Enthalpy of Wall using Stanton Number
Go
Verified
Nusselt Number for Hypersonic Vehicle
Go
6 More Local Heat Transfer for Hypersonic Flow Calculators
Go
Nonlifting Flow over Cylinder
(5)
Created
Radial Velocity for Non-Lifting Flow over Circular Cylinder
Go
Created
Radius of Cylinder for Non-Lifting Flow
Go
Created
Stream Function for Non-Lifting Flow over Circular Cylinder
Go
Created
Surface Pressure Coefficient for Non-Lifting Flow over Circular Cylinder
Go
Created
Tangential Velocity for Non-Lifting Flow over Circular Cylinder
Go
5 More Nonlifting Flow over Cylinder Calculators
Go
Normal Shock Relations
(2)
Created
Critical Speed of Sound from Prandtl Relation
Go
Created
Upstream Velocity using Prandtl Relation
Go
5 More Normal Shock Relations Calculators
Go
Number of Connectors in Bridges
(5)
Verified
Effective Concrete Area given Force in Slab
Go
Verified
Force in Slab at Maximum Positive Moments given Minimum Number of Connectors for Bridges
Go
Verified
Force in Slab given Effective Concrete Area
Go
Verified
Minimum Number of Connectors for Bridges
Go
Verified
Steel Yield Strength given Total Area of Steel Section
Go
13 More Number of Connectors in Bridges Calculators
Go
Oblique Shock
(7)
Created
Component of Downstream Mach Number Normal to Oblique Shock for given Normal Upstream Mach Number
Go
Created
Density behind Oblique Shock for given Upstream Density and Normal Upstream Mach Number
Go
Created
Density Ratio across Oblique Shock
Go
Created
Pressure behind Oblique Shock for given Upstream Pressure and Normal Upstream Mach Number
Go
Created
Pressure Ratio across Oblique Shock
Go
Created
Temperature behind Oblique Shock for given Upstream Temperature and Normal Upstream Mach Number
Go
Created
Temperature Ratio across Oblique Shock
Go
3 More Oblique Shock Calculators
Go
Planar and Blunt Slab Blast Wave
(1)
Verified
Pressure Ratio for Blunt Cylinder Blast Wave
Go
7 More Planar and Blunt Slab Blast Wave Calculators
Go
Power Transmission
(2)
Verified
Efficiency of Power Transmission through Nozzle
Go
Verified
Efficiency of power transmission through nozzle for velocity and total head
Go
3 More Power Transmission Calculators
Go
Preliminary Aerodynamics
(3)
Verified
Power required at sea-level conditions
Go
Verified
Velocity at Altitude given Velocity at Sea-Level
Go
Verified
Velocity at Sea-Level given Lift Coefficient
Go
14 More Preliminary Aerodynamics Calculators
Go
Pressure and Flow Head
(2)
Verified
Loss of Head at Entrance of Pipe
Go
Verified
Loss of head in equivalent pipe
Go
12 More Pressure and Flow Head Calculators
Go
Property Change Across Shock Waves
(4)
Created
Density Ratio across Normal Shock
Go
Created
Pressure Ratio across Normal Shock
Go
Created
Static Enthalpy Ratio across Normal Shock
Go
Created
Temperature Ratio across Normal Shock
Go
2 More Property Change Across Shock Waves Calculators
Go
Pull Up and Pull Down Maneuver
(1)
Verified
Velocity given Pull-down Maneuver Radius
Go
11 More Pull Up and Pull Down Maneuver Calculators
Go
Reference Temperature Method
(1)
Verified
Overall Skin-Friction Drag Coefficient
Go
14 More Reference Temperature Method Calculators
Go
Resultants and Stress
(4)
Created
Normal rake angle for given Resultant force, force along shear, shear, and friction angle
Go
Created
R in merchant circle for given force along shear force, shear, friction and normal rake angles
Go
Created
Resultant force in merchant circle for given cutting force, friction and normal rake angles
Go
Created
Shear stress given cutting force, cut size, uncut chip thickness, friction, rake and shear angles
Go
2 More Resultants and Stress Calculators
Go
Shear Range
(1)
Verified
Horizontal Shear Range at Juncture of Slab and Beam
Go
11 More Shear Range Calculators
Go
Shock Dynamics and Aerodynamic Shape
(3)
Verified
Local Shock Velocity Equation
Go
Verified
Mach Wave behind Shock
Go
Verified
Mach Wave behind Shock with Mach Infinity
Go
7 More Shock Dynamics and Aerodynamic Shape Calculators
Go
Source Flow
(7)
Created
Radial Velocity for 2-D Incompressible Source Flow
Go
Created
Source Strength for 2-D Incompressible Source Flow
Go
Created
Stagnation Streamline Equation for Flow over Semi-Infinite Body
Go
Created
Stream Function for 2-D Incompressible Source Flow
Go
Created
Stream Function for Flow over Rankine Oval
Go
Created
Stream Function for Semi-Infinite Body
Go
Created
Velocity Potential for 2-D Source Flow
Go
Space Marching Finite Difference Method Additional Solutions of the Euler Equations
(3)
Verified
Enthalpy Equation using Coefficient of Pressure for Calorically Perfect Gas
Go
Verified
Free Stream Enthalpy
Go
Verified
Total Specific Enthalpy
Go
8 More Space Marching Finite Difference Method Additional Solutions of the Euler Equations Calculators
Go
Stick Forces and Hinge Moments
(6)
Verified
Elevator Chord Length given Hinge Moment Coefficient
Go
Verified
Elevator Deflection Angle for given Stick Force
Go
Verified
Elevator Stick Force
Go
Verified
Elevator Stick Force given Hinge Moment Coefficient
Go
Verified
Gearing Ratio for given Stick Force
Go
Verified
Stick Deflection Angle for given Gearing Ratio
Go
17 More Stick Forces and Hinge Moments Calculators
Go
Tail Contribution
(7)
Verified
Horizontal tail area for given tail volume ratio
Go
Verified
Horizontal tail volume ratio
Go
Verified
Pitching Moment due to Tail
Go
Verified
Tail moment arm for given horizontal tail volume ratio
Go
Verified
Tail Pitching Moment for given Moment Coefficient
Go
Verified
Wing Mean Aerodynamic Chord for given Horizontal Tail Volume Ratio
Go
Verified
Wing Reference Area for given Horizontal Tail Volume Ratio
Go
12 More Tail Contribution Calculators
Go
Take Off
(10)
Verified
Coefficient of rolling friction during ground roll
Go
Verified
Drag during ground effect
Go
Verified
Ground effect factor
Go
Verified
Lift acting on aircraft during ground roll
Go
Verified
Liftoff distance
Go
Verified
Maximum Lift coefficient for given liftoff velocity
Go
Verified
Resistance force during ground roll
Go
Verified
Stall velocity for given weight
Go
Verified
Thrust for given liftoff distance
Go
Verified
Weight of aircraft during ground roll
Go
5 More Take Off Calculators
Go
Turbulent Flow
(3)
Verified
Average Height of Irregularities for Turbulent Flow in Pipes
Go
Verified
Power Required to Maintain Turbulent Flow
Go
Verified
Roughness Reynold Number for Turbulent Flow in Pipes
Go
15 More Turbulent Flow Calculators
Go
Turning Flight
(7)
Verified
Bank angle during level turn
Go
Verified
Load factor given Lift Force and Weight of Aircraft
Go
Verified
Load Factor given Turn Radius
Go
Verified
Turn rate
Go
Verified
Velocity for given turn radius
Go
Verified
Velocity for given turn rate
Go
Verified
Weight for given Load Factor
Go
6 More Turning Flight Calculators
Go
Ultimate Shear Strength of Connectors in Bridges
(3)
Verified
Channel Web Thickness given Ultimate Shear Connector Strength for Channels
Go
Verified
Elastic Modulus of Concrete given Ultimate Shear Connector Strength for Welded Studs
Go
Verified
Ultimate Shear Strength for Welded Studs
Go
6 More Ultimate Shear Strength of Connectors in Bridges Calculators
Go
Uniform Flow
(4)
Created
Stream Function for Uniform Incompressible Flow
Go
Created
Stream Function for Uniform Incompressible Flow in Polar Coordinates
Go
Created
Velocity Potential for Uniform Incompressible Flow
Go
Created
Velocity Potential for Uniform Incompressible Flow in Polar Coordinates
Go
Upstream Shock Waves
(5)
Created
Density ahead of Normal Shock using Normal Shock Momentum Equation
Go
Created
Enthalpy ahead of Normal Shock from Normal Shock Energy Equation
Go
Created
Static Pressure ahead of Normal Shock using Normal Shock Momentum Equation
Go
Created
Velocity ahead of Normal Shock by Normal Shock Momentum Equation
Go
Created
Velocity ahead of Normal Shock from Normal Shock Energy Equation
Go
2 More Upstream Shock Waves Calculators
Go
Vertical Tail Contribution
(8)
Verified
Moment Produced by Vertical Tail for given Moment Coefficient
Go
Verified
Moment Produced by Vertical Tail for given Side Force
Go
Verified
Vertical Tail Angle of Attack
Go
Verified
Vertical tail area for given vertical tail volume ratio
Go
Verified
Vertical Tail Moment Arm for given Side Force
Go
Verified
Vertical Tail Moment Arm for given Vertical Tail Volume Ratio
Go
Verified
Vertical Tail Side Force for Given Moment
Go
Verified
Vertical tail volume ratio
Go
16 More Vertical Tail Contribution Calculators
Go
Viscous Flow
(1)
Verified
Total Enthalpy in Inviscid Flow Outside Boundary Layer
Go
14 More Viscous Flow Calculators
Go
Vortex Flow
(3)
Created
Stream Function for 2-D Vortex Flow
Go
Created
Tangential Velocity for 2-D Vortex Flow
Go
Created
Velocity Potential for 2-D Vortex Flow
Go
Wing Tail Contribution
(3)
Verified
Angle of Attack at Tail
Go
Verified
Downwash angle
Go
Verified
Total Lift Coefficient of Wing-Tail Combination
Go
12 More Wing Tail Contribution Calculators
Go
Wing Tail Interaction
(2)
Verified
Wing Area for given Vertical Tail Volume Ratio
Go
Verified
Wingspan for given Vertical Tail Volume Ratio
Go
10 More Wing Tail Interaction Calculators
Go
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