Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ 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

11 Other formulas that calculate the same Output

Drag during ground effect
Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area) GO
Drag in an accelerated flight
Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) GO
Drag force on the plate in boundary layer flow
Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number) GO
Drag force in falling sphere resistance method
Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere GO
Forces acting on body along the flight path
Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient) GO
Drag for a level, unaccelerated flight
Drag Force=Thrust of an aircraft*(cos(Thrust angle)) GO
Drag for a level, unaccelerated flight at negligible thrust angle
Drag Force=Dynamic Pressure*Area*Drag Coefficient GO
Drag force
Drag Force=Drag Coefficient*Dynamic Pressure*Area GO
Total Drag for given excess power
Drag Force=Thrust force-(Excess Power/Velocity) GO
Drag force with angle of attack
Drag Force=Lift force/cot(Angle of attack) GO
Drag for given glide angle
Drag Force=Lift force*tan(Glide angle) GO

Total drag for given required power Formula

Drag Force=Power/Freestream Velocity
F<sub>D</sub>=P/V<sub>∞</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
Freestream Velocity for given total drag GO

What is Drag?

Drag is the aerodynamic force that opposes an aircraft's motion through the air. Drag is generated by every part of the airplane (even the engines!).

How to Calculate Total drag for given required power?

Total drag for given required power calculator uses Drag Force=Power/Freestream Velocity to calculate the Drag Force, The Total drag for given required power in a steady, level flight is equal to the ratio of required power and freestream velocity. . Drag Force and is denoted by FD symbol.

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

FAQ

What is Total drag for given required power?
The Total drag for given required power in a steady, level flight is equal to the ratio of required power and freestream velocity. and is represented as FD∞ or Drag Force=Power/Freestream Velocity. Power is the amount of energy liberated per second in a device and The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.
How to calculate Total drag for given required power?
The Total drag for given required power in a steady, level flight is equal to the ratio of required power and freestream velocity. is calculated using Drag Force=Power/Freestream Velocity. To calculate Total drag for given required power, you need Power (P) and Freestream Velocity (V). With our tool, you need to enter the respective value for Power and Freestream Velocity 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 Drag Force?
In this formula, Drag Force uses Power and Freestream Velocity. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Drag Force=Drag Coefficient*Dynamic Pressure*Area
  • Drag Force=(Weight*sin(Angle of Inclination))-(Mass*Velocity Gradient)
  • Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration)
  • Drag Force=Thrust of an aircraft*(cos(Thrust angle))
  • Drag Force=Dynamic Pressure*Area*Drag Coefficient
  • Drag Force=Lift force/cot(Angle of attack)
  • Drag Force=Thrust force-(Excess Power/Velocity)
  • Drag Force=Lift force*tan(Glide angle)
  • Drag Force=(Parasite Drag coefficient+(((lift coefficient^2)*Ground effect factor)/(pi*Oswald efficiency factor*Aspect Ratio of a wing)))*(0.5*Freestream density*(Velocity^2)*Reference Area)
  • Drag Force=3*pi*viscosity of fluid*velocity of sphere*diameter of sphere
  • Drag Force=0.73*Width*viscosity of fluid*Fluid Velocity*sqrt(Reynolds Number)
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