Calculate True Airspeed of Airplane

 Method to Calculate the True Airspeed of an Airplane

• Calculate Continuity Equation for Incompressible Flow

• Calculate Continuity Equation for Compressible Flow

• Calculate Bernoulli's Equation

• Calculate Pressure at Exit of Convergent Duct

• Isentropic Flow Calculations

• Calculate Velocity at Throat of Supersonic Wind Tunnel

• Calculate Velocity at Exit of Supersonic Wind Tunnel

• Calculate Area at Throat and Exit of Supersonic Wind Tunnel

• Calculate Local Shear Stress in Laminar Flow Direction

• Calculate Local Shear Stress in Turbulent Flow Direction

• Calculate Airflow Velocity in Test Section of Subsonic Wind Tunnel

• Calculate True Velocity of an Airplane

• Calculate Equivalent Airspeed of an Airplane

• Calculate Reservoir Pressure for Supersonic Wind Tunnel

• Calculate Temperature Area Ratio for Supersonic Wind Tunnel

• Calculate Pressure at Stagnation Point

• Calculate Temperature at Stagnation Point

• Calculate Density at Stagnation Point

• Calculate Mass Flow through the Nozzle

• Calculate Velocity at a point on an Airfoil

• Calculate Mach Number

• Calculate Mach Number of Flow at Nozzle

• Calculate Mach Number of Flow at Exit

• Calculate True Airspeed

• Calculate Calibrated Airspeed

• Calculate Pressure Measured by Pitot Tube

• Calculate Boundary Layer Thickness at Trailing Edge

• Calculate Drag force on Plate

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How to Calculate the True Airspeed of the Airplane

In order to calculate the True Airspeed of the Airplane we require the altitude at which the airplane is flying from which we extract the temperature value at that altitude in Kelvin (K).

Furthermore, we require the pressure measured by the Pitot Tube in N/m^2.

And the Ambient value of the temperature in Kelvin (K).

Performing the calculation, gives us,

the Speed of sound at that altitude and

the true Airspeed Vtrue of the Airplane in m/s.

Download Free Program to Calculate the True Airspeed