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Telangana State Post Graduate Engineering Common Entrance Test
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Aerospace Engineering
List of top Aerospace Engineering Questions asked in Telangana State Post Graduate Engineering Common Entrance Test
The shape of Rankine oval of equal axes can be found out by substituting
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
When the velocity at the wall is zero, it refers to
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
In a flow, if velocity potential (\(\phi\)) exists, then the flow is said to be
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
Stream function is defined for
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
Circulation is referred to as
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
If \(\nabla \times \mathbf{V} = 0\), then the flow is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
The drag due to the pressure distribution around the wing is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
The continuum approach breaks down when the mean free path of the molecules is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
For a given chamber pressure, the thrust of a rocket engine is highest when
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Rocket Propulsion
The life of a geostationary communication satellite is limited by
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
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
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
An artificial satellite remains in orbit and does not fall on to the Earth because
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
If the wind reference line coincides with the relative wind direction, then the axis system refers to
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
Which one of the following is true with respect to the phugoid mode of an aircraft?
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Dynamic Stability
Control of hinge moment parameters is called
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerofoils and Wings
Aileron reversal speed can be increased by
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerofoils and Wings
The rolling moment due to side slip is called
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aircraft Stability
The control surface associated with engine inoperative condition is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Airplane Performance
For an airplane to be statically stable, its centre of gravity must always be
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aircraft Stability
The lift acting on an aircraft climbing vertically up is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
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
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Airplane Performance
A conventional Altimeter is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Airplane Performance
The drag of an aircraft in steady climbing flight at a given forward speed is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
The service ceiling of transport aircraft is the altitude
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Airplane Performance
The minimum glide angle of the unpowered flight depends on
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
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