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Calculate Rate of Climb R/C for Single Engine Propeller Airplane Method to Compute the Rate of Climb (R/C) for Single Engine Propeller Driven Airplane 

Aerospace



Rate of Climb R/C for Single Engine Propeller Airplane In order to compute the Rate of Climb R/C for Single engine propeller driven airplane we need to have certain parameters. 

The parameters include,
The Wing span in feet. The Wing Area if feet^2/sec. The Normal Gross Weight of the Airplane in pounds lb. The fuel capacity of the Airplane in gallons (gal) of aviation gasoline. The Powerplant / Engine Hourse Power value (hp). The Specific Fuel Consumption Value in lb/ (hp)(h) The Parasite Drag Coefficient of the Airplane Cd,0 value. The Value of the Oswald Efficiency Factor, e. The Value of the Propeller Efficiency And the Assumed Velocity in feet /sec.


Performing the calculation,
Download Free Program to Calculate the Rate of Climb R/C of a Propeller Driven Airplane

