The pitch rate of an aircraft is a rate of change of the aircraft orientation with respect to an inertial frame, expressed in body axes
Category: Aircraft Design
Where:-
a0 is the Speed of Sound at standard Sea level = 661.478 KT
M is the Mach Number
T is the Temperature in Kelvin
T0 is the Standard sea level Temperature (288.15 Kelvin)
True Airspeed of an Aircraft is a speed Relative to the air mass through which Aircraft is Flying.
Chandan Singh
Where:-
D is the Drag
V is the Velocity of Aircraft
ηp is the Efficiency of Propeller
Brake horse Power (BHP) is the Power actually delivered by the engine and is therefore the capacity of the engine. The power developed in the combustion chambers of the engine is greater than the delivered power because of friction and other mechanical losses.
Chandan Singh
Vertical tail volume ratio is the relation between tail volume and wing volume. Vertical tail contributes positively for Directional Stability. Its SI unit is dimensionless.
