Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
Sanjay Krishna 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

9 Other formulas that calculate the same Output

Weight of aircraft during ground roll
Weight=(Rolling Resistance/Coefficient of Rolling Friction)+Lift force GO
Weight of aircraft for given coefficients of lift and drag
Weight=lift coefficient*Thrust of an aircraft/Drag Coefficient GO
Weight of aircraft in level, unaccelerated flight
Weight=Lift force+(Thrust of an aircraft*sin(Thrust angle)) GO
Weight of aircraft for given Lift-to-drag ratio
Weight=Thrust of an aircraft*Lift-to-drag ratio GO
Weight of aircraft for a level, unaccelerated flight at negligible thrust angle
Weight=Dynamic Pressure*Area*lift coefficient GO
Total weight of the ram of hydraulic accumulator
Weight=Pressure intensity*Area of sliding ram GO
Weight of aircraft for given excess power
Weight=Excess Power/Rate of Climb GO
Weight during level turn
Weight=Lift force*cos(Bank angle) GO
Weight for a given load factor
Weight=Lift force/Load factor GO

Weight of aircraft for given required power Formula

Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient)
W=P*C<sub>L</sub>/(V<sub>∞</sub>*C<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
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
Freestream Velocity for given total drag GO

What is aircraft gross weight?

The aircraft gross weight (also known as the all-up weight and abbreviated AUW) is the total aircraft weight at any moment during the flight or ground operation.

How to Calculate Weight of aircraft for given required power?

Weight of aircraft for given required power calculator uses Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient) to calculate the Weight, The Weight of aircraft for given required power in a steady, level flight is a function of freestream velocity and aerodynamic coefficients. Weight and is denoted by W symbol.

How to calculate Weight of aircraft for given required power using this online calculator? To use this online calculator for Weight of aircraft for given required power, enter Power (P), lift coefficient (CL), Freestream Velocity (V) and Drag Coefficient (CD) and hit the calculate button. Here is how the Weight of aircraft for given required power calculation can be explained with given input values -> 0.1 = 100*10/(100*100).

FAQ

What is Weight of aircraft for given required power?
The Weight of aircraft for given required power in a steady, level flight is a function of freestream velocity and aerodynamic coefficients and is represented as W=P*CL/(V*CD) or Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient). Power is the amount of energy liberated per second in a device, The lift coefficient (CL) is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. , 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 and Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
How to calculate Weight of aircraft for given required power?
The Weight of aircraft for given required power in a steady, level flight is a function of freestream velocity and aerodynamic coefficients is calculated using Weight=Power*lift coefficient/(Freestream Velocity*Drag Coefficient). To calculate Weight of aircraft for given required power, you need Power (P), lift coefficient (CL), Freestream Velocity (V) and Drag Coefficient (CD). With our tool, you need to enter the respective value for Power, lift coefficient, Freestream Velocity and Drag Coefficient 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 Weight?
In this formula, Weight uses Power, lift coefficient, Freestream Velocity and Drag Coefficient. We can use 9 other way(s) to calculate the same, which is/are as follows -
  • Weight=Lift force+(Thrust of an aircraft*sin(Thrust angle))
  • Weight=Dynamic Pressure*Area*lift coefficient
  • Weight=lift coefficient*Thrust of an aircraft/Drag Coefficient
  • Weight=Thrust of an aircraft*Lift-to-drag ratio
  • Weight=Excess Power/Rate of Climb
  • Weight=(Rolling Resistance/Coefficient of Rolling Friction)+Lift force
  • Weight=Lift force*cos(Bank angle)
  • Weight=Lift force/Load factor
  • Weight=Pressure intensity*Area of sliding ram
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