List of top Aerospace Engineering Questions

Which of the following instrument is used to indicate air speed corrected for compressibility effect?
True airspeed (TAS) is \[ (\rho_0 = \text{Air density at sea level},\ \rho = \text{Air density through which aircraft flying}) \]
What is the percentage of increment in lift produced by two main wings when compared to monoplane of similar aircraft?
Winds in which the Coriolis force is equal and opposite to the pressure-gradient force are called:
For the aircraft, the angle between the relative velocity vector and the chord line is
For the neutrally stable state of the atmosphere, the adiabatic lapse rate is
A liquid-propellant rocket engine is used to develop a thrust of 1.5 kN with a characteristic velocity of 1900 m/s at chamber pressure of 5 MPa. If its thrust coefficient CF happens to be 1.2, then the throat of nozzle is
If the load passes through the shear center of the section of a beam, then there will be
A small rocket having a specific impulse of 200s produces a total thrust of 980 N, out of which 100N is the pressure thrust. Considering the acceleration due to gravity to be $9.8~m/s^2$, the propellant mass flow rate in kg/s is
The dutch roll mode of the aircraft can be excited by applying