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

Thrust in an accelerated flight
Thrust of an aircraft=(sec(Thrust angle))*(Drag Force+(Mass*[g]*sin(Flight path angle))+(Mass*Acceleration)) GO
Drag in an accelerated flight
Drag Force=(Thrust of an aircraft*cos(Thrust angle))-(Mass*[g]*(sin(Flight path angle)))-(Mass*Acceleration) GO
Weight of aircraft for given coefficients of lift and drag
Weight=lift coefficient*Thrust of an aircraft/Drag Coefficient GO
Lift for an unaccelerated flight
Lift force=Weight-(Thrust of an aircraft*sin(Thrust angle)) GO
Thrust angle for an unaccelerated flight for given lift
Thrust angle=asin((Weight-Lift force)/Thrust of an aircraft) GO
Weight of aircraft in level, unaccelerated flight
Weight=Lift force+(Thrust of an aircraft*sin(Thrust angle)) GO
Thrust for a level, unaccelerated flight
Thrust of an aircraft=Drag Force/(cos(Thrust angle)) GO
Drag for a level, unaccelerated flight
Drag Force=Thrust of an aircraft*(cos(Thrust angle)) GO
Coefficient of drag
Drag Coefficient=Drag Force/(Dynamic Pressure*Area) GO
Dynamic pressure
Dynamic Pressure=Drag Force/(Drag Coefficient*Area) GO
Thrust angle for an unaccelerated flight for given drag
Thrust angle=acos(Drag Force/Thrust force) GO

11 Other formulas that calculate the same Output

Velocity of the follower after time t (Cycloidal motion)
Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke)))) GO
Velocity of the follower for tangent cam with roller follower(contact with straight flanks)
Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2)) GO
Velocity OF A Progressive Wave
Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave GO
Velocity Of The Particle
Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi) GO
Velocity due to voltage
Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e]) GO
Velocity Of Wave in String
Velocity=sqrt(Tension Of String/Mass Per Unit length) GO
Velocity OF A Progressive Wave(Using Angular Frequency)
Velocity=(Wavelength*Angular Frequency)/(4*pi) GO
Velocity OF A Progressive Wave(Using Frequency)
Velocity=Wavelength Of A Wave*frequency GO
Velocity Of A Wave(Using Wave Number)
Velocity=Angular Frequency/Wave Number GO
Velocity Of Sound In Liquid
Velocity=sqrt(bulk modulus/Density) GO
Velocity Of Sound In Solids
Velocity=sqrt(Elasticity/Density) GO

Velocity of aircraft for given excess power Formula

Velocity=Excess Power/(Thrust of an aircraft-Drag Force)
v=P<sub>excess</sub>/(T-F<sub>D</sub>)
More formulas
Rate of Climb GO
Velocity of aircraft at a given rate of climb GO
Flight path angle at a given rate of climb GO
Excess power GO
Thrust available for given excess power GO
Total Drag for given excess power GO
Rate of Climb for given excess power GO
Excess power for given rate of climb GO
Weight of aircraft for given excess power GO

How do aircraft performance parameters vary?

The variation of aircraft performance parameters such as climb rate, acceleration capability, range varies significantly based on aircraft speed and altitude.

How to Calculate Velocity of aircraft for given excess power?

Velocity of aircraft for given excess power calculator uses Velocity=Excess Power/(Thrust of an aircraft-Drag Force) to calculate the Velocity, The Velocity of aircraft for given excess power is given by the excess power divided by the difference between available thrust and total drag. Velocity and is denoted by v symbol.

How to calculate Velocity of aircraft for given excess power using this online calculator? To use this online calculator for Velocity of aircraft for given excess power, enter Excess Power (Pexcess), Thrust of an aircraft (T) and Drag Force (FD and hit the calculate button. Here is how the Velocity of aircraft for given excess power calculation can be explained with given input values -> NaN = 1500/(100-100).

FAQ

What is Velocity of aircraft for given excess power?
The Velocity of aircraft for given excess power is given by the excess power divided by the difference between available thrust and total drag and is represented as v=Pexcess/(T-FD or Velocity=Excess Power/(Thrust of an aircraft-Drag Force). Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft, The Thrust of an aircraft is defined as the force generated through propulsion engines that move an aircraft through the air and Drag Force is the resisting force experienced by an object moving through a fluid.
How to calculate Velocity of aircraft for given excess power?
The Velocity of aircraft for given excess power is given by the excess power divided by the difference between available thrust and total drag is calculated using Velocity=Excess Power/(Thrust of an aircraft-Drag Force). To calculate Velocity of aircraft for given excess power, you need Excess Power (Pexcess), Thrust of an aircraft (T) and Drag Force (FD. With our tool, you need to enter the respective value for Excess Power, Thrust of an aircraft 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 Velocity?
In this formula, Velocity uses Excess Power, Thrust of an aircraft and Drag Force. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Velocity=Wavelength Of A Wave/Time Period Of Progressive Wave
  • Velocity=Wavelength Of A Wave*frequency
  • Velocity=(Wavelength*Angular Frequency)/(4*pi)
  • Velocity=Angular Frequency/Wave Number
  • Velocity=sqrt(Tension Of String/Mass Per Unit length)
  • Velocity=sqrt(bulk modulus/Density)
  • Velocity=sqrt(Elasticity/Density)
  • Velocity=sqrt((2*[Charge-e]*Velocity of electron)/[Mass-e])
  • Velocity=(Quantum Number*Plancks Constant)/(Mass*Radius*2*pi)
  • Velocity=((Angular velocity of the cam*Stroke of the follower)/Angular displacement of the cam during out stroke)*(1-(cos((2*pi*Angle through which the cam rotates)/(Angular displacement of the cam during out stroke))))
  • Velocity=Angular velocity of the cam*(Radius of the base circle+Radius of the roller)*(sin(Angle turned by cam from beginning of roller)/((cos(Angle turned by cam from beginning of roller))^2))
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