Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 200+ more calculators!
Sai Venkata Phanindra Chary Arendra
Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad
Sai Venkata Phanindra Chary Arendra has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Torque transmitted if power is known for epicyclic-train dynamometer
Torque=(Power*60)/(2*pi* Speed of the shaft in rpm) GO
Indicated Thermal Efficiency
indicated thermal efficiency=Power/Energy Required GO
Brake Thermal Efficiency
brake thermal efficiency=Power/Energy Required GO
Voltage When The Power Factor Is Given
Voltage=Power/(Power Factor*Electric Current) GO
Current When The Power Factor Is Given
Electric Current=Power/(Power Factor*Voltage) GO
Power Factor When Power Is Given
Power Factor=Power/(Voltage*Electric Current) GO
Armature Current When Power Is Given
Armature Current=Power/Induced voltage GO
Induced Voltage When Power Is Given
Induced voltage=Power/Armature Current GO
Force By A Linear Induction Motor
Force=Power/Linear Synchronous Speed GO
Intensity Of Sound
Resultant Intensity=Power*Area GO
Angular Speed Of Series DC Generator Using Generated Power
Angular Speed=Power/Torque GO

5 Other formulas that calculate the same Output

Freestream velocity for local drag coefficient in boundary layer flows
Freestream Velocity=sqrt(Shear Stress/(0.5*density of fluid*local coefficient of drag)) GO
Freestream velocity for lift coefficient in a rotating cylinder with circulation
Freestream Velocity=Circulation/(Cylinder Radius*lift coefficient) GO
Freestream velocity for lift coefficient with tangential speed
Freestream Velocity=(2*pi*Tangential Velocity)/lift coefficient GO
Freestream velocity for a single stagnation point
Freestream Velocity=Circulation/(4*pi*Cylinder Radius) GO
Freestream velocity for given required power
Freestream Velocity=Power/Thrust of an aircraft GO

Freestream Velocity for given total drag Formula

Freestream Velocity=Power/Drag Force
V<sub>∞</sub>=P/F<sub>D</sub>
More formulas
Power required for given required thrust GO
Thrust required for given required power GO
Freestream velocity for given required power GO
Power required for given aerodynamic coefficients GO
Weight of aircraft for given required power GO
Zero-lift drag coefficient for minimum power required GO
Coefficient of Drag due to lift for minimum power required GO
Power required for given total drag GO
Total drag for given required power GO

How is freestream velocity measured?

In real-time measurements, the freestream velocity is measured through Pitot tubes. They are usually located either under the wing or right after the cabin of the airplane.

How to Calculate Freestream Velocity for given total drag?

Freestream Velocity for given total drag calculator uses Freestream Velocity=Power/Drag Force to calculate the Freestream Velocity, The Freestream Velocity for given total drag in a steady, level flight is equal to the ratio of required power and total drag force of an aircraft. Freestream Velocity and is denoted by V symbol.

How to calculate Freestream Velocity for given total drag using this online calculator? To use this online calculator for Freestream Velocity for given total drag, enter Power (P) and Drag Force (FD and hit the calculate button. Here is how the Freestream Velocity for given total drag calculation can be explained with given input values -> 1 = 100/100.

FAQ

What is Freestream Velocity for given total drag?
The Freestream Velocity for given total drag in a steady, level flight is equal to the ratio of required power and total drag force of an aircraft and is represented as V=P/FD or Freestream Velocity=Power/Drag Force. Power is the amount of energy liberated per second in a device and Drag Force is the resisting force experienced by an object moving through a fluid.
How to calculate Freestream Velocity for given total drag?
The Freestream Velocity for given total drag in a steady, level flight is equal to the ratio of required power and total drag force of an aircraft is calculated using Freestream Velocity=Power/Drag Force. To calculate Freestream Velocity for given total drag, you need Power (P) and Drag Force (FD. With our tool, you need to enter the respective value for Power and Drag Force and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
How many ways are there to calculate Freestream Velocity?
In this formula, Freestream Velocity uses Power and Drag Force. We can use 5 other way(s) to calculate the same, which is/are as follows -
  • Freestream Velocity=Power/Thrust of an aircraft
  • Freestream Velocity=sqrt(Shear Stress/(0.5*density of fluid*local coefficient of drag))
  • Freestream Velocity=Circulation/(Cylinder Radius*lift coefficient)
  • Freestream Velocity=(2*pi*Tangential Velocity)/lift coefficient
  • Freestream Velocity=Circulation/(4*pi*Cylinder Radius)
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