List of top Aerospace Engineering Questions asked in TS PGECET

If \(\nabla \times \mathbf{V} = 0\), then the flow is
The drag due to the pressure distribution around the wing is
The continuum approach breaks down when the mean free path of the molecules is
For a given chamber pressure, the thrust of a rocket engine is highest when
The life of a geostationary communication satellite is limited by
To transfer a satellite from an elliptical orbit into a circular orbit having a radius equal to the apogee distance of the elliptical orbit, then the speed of the satellite should be
An artificial satellite remains in orbit and does not fall on to the Earth because
If the wind reference line coincides with the relative wind direction, then the axis system refers to
Which one of the following is true with respect to the phugoid mode of an aircraft?
Control of hinge moment parameters is called
Aileron reversal speed can be increased by
The rolling moment due to side slip is called
The control surface associated with engine inoperative condition is
For an airplane to be statically stable, its centre of gravity must always be
The lift acting on an aircraft climbing vertically up is
If an aircraft is climbing at a constant speed in a straight line at a steep angle of climb, the load factor it sustains during the climb is
A conventional Altimeter is
The drag of an aircraft in steady climbing flight at a given forward speed is
The service ceiling of transport aircraft is the altitude
The minimum glide angle of the unpowered flight depends on
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