The landing-gear WERs typically used for manned |
Category: Airplane Performance Calculator
This category helps you to calculate the airplane performance numerical like velocity, take-off distance, climb rate, turn radius, etc., – WINGS OF AERO
The gross thrust coefficient (Cfg) is a measure of the nozzle efficiency and accounts for nozzle losses due to friction, angularity, expansion, leakage and cooling air throttling
The Mach number of a normal shock wave is always greater than unity in the upstream and less than unity in the downstream, the static pressure always increases across the shock wave
Mx= Up Stream Mach Number
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
