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

Minimum Thrust required for given weight
Thrust of an aircraft=(Dynamic Pressure*Reference Area*Zero-lift drag coefficient)+((Weight^2)/(Dynamic Pressure*Reference Area*pi*Oswald efficiency factor*Aspect Ratio of a wing)) GO
Power required at sea-level condition
Power required at sea-level=sqrt(2*(Weight^3)*(Drag Coefficient^2)/([Std-Air-Density-Sea]*Reference Area*(lift coefficient^3))) GO
Velocity at sea-level condition
Velocity at sea-level=sqrt(2*Weight/([Std-Air-Density-Sea]*Reference Area*lift coefficient)) GO
Power required for given aerodynamic coefficients
Power=Weight*Freestream Velocity*Drag Coefficient/lift coefficient GO
Coefficient of Drag for given thrust and weight
Drag Coefficient=Thrust of an aircraft*lift coefficient/Weight GO
Coefficient of Lift for given thrust and weight
lift coefficient=Weight*Drag Coefficient/Thrust of an aircraft GO
Thrust for given coefficients of lift and drag
Thrust of an aircraft=Drag Coefficient*Weight/lift 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
Thrust required for given Lift-to-drag ratio
Thrust of an aircraft=Weight/Lift-to-drag ratio GO
Lift-to-drag ratio for given required thrust
Lift-to-drag ratio=Weight/Thrust of an aircraft GO

1 Other formulas that calculate the same Output

Rate of Climb
Rate of Climb=Velocity*sin(Flight path angle) GO

Rate of Climb for given excess power Formula

Rate of Climb=Excess Power/Weight
R/C=P<sub>excess</sub>/W
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
Velocity of aircraft for given excess power GO
Excess power for given rate of climb GO
Weight of aircraft for given excess power GO

What is the best angle of climb speed?

The best angle of climb speed of an aircraft gets you the greatest altitude per unit of ground distance (feet per mile).

How to Calculate Rate of Climb for given excess power?

Rate of Climb for given excess power calculator uses Rate of Climb=Excess Power/Weight to calculate the Rate of Climb, The Rate of Climb for given excess power of an aircraft is defined as the ratio of excess power and weight of the aircraft. Rate of Climb and is denoted by R/C symbol.

How to calculate Rate of Climb for given excess power using this online calculator? To use this online calculator for Rate of Climb for given excess power, enter Excess Power (Pexcess) and Weight (W) and hit the calculate button. Here is how the Rate of Climb for given excess power calculation can be explained with given input values -> 15 = 1500/100.

FAQ

What is Rate of Climb for given excess power?
The Rate of Climb for given excess power of an aircraft is defined as the ratio of excess power and weight of the aircraft and is represented as R/C=Pexcess/W or Rate of Climb=Excess Power/Weight. Excess Power is defined as the difference between the power available and the power required at a particular speed and altitude of aircraft and Weight is a vector quantity and defined as the product of mass and acceleration acting on that mass.
How to calculate Rate of Climb for given excess power?
The Rate of Climb for given excess power of an aircraft is defined as the ratio of excess power and weight of the aircraft is calculated using Rate of Climb=Excess Power/Weight. To calculate Rate of Climb for given excess power, you need Excess Power (Pexcess) and Weight (W). With our tool, you need to enter the respective value for Excess Power and Weight 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 Rate of Climb?
In this formula, Rate of Climb uses Excess Power and Weight. We can use 1 other way(s) to calculate the same, which is/are as follows -
  • Rate of Climb=Velocity*sin(Flight path angle)
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