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Telangana State Post Graduate Engineering Common Entrance Test
List of top Questions asked in Telangana State Post Graduate Engineering Common Entrance Test
The velocity induced at a point \(P\) by the semi-infinite vortex filament is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
In thin airfoil theory the lift curve slope is usually considered as
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
According to Kutta condition, if the trailing edge is cusped, then the velocities leaving the top (\(V_1\)) and bottom (\(V_2\)) surfaces at the trailing edge should be
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
In lifting flow over a cylinder the location of stagnation points when \(\Gamma = 4\pi U R\) is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
The velocity potential \(\phi\) for a vortex flow is given by
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
Fire Stoke’s 1st comparison of pressure forces and friction forces acting on any given fluid element shows that
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
The incompressible continuity equation in polar coordinates is written as
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Fluid Mechanics
Kutta-Joukowski’s theorem is defined for
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
The amount of lift generated in the non-rotating flow over a circular cylinder is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
At low values of incidence, the center of pressure
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
The aerodynamic center on the aerofoil is the point where
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
The profile drag for a two-dimensional aerofoil is
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Aerodynamics
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
Proteomics refers to the study of
TS PGECET - 2024
TS PGECET
Biotechnology
Bioinformatics and Genomics
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
Which of the following is not a variant of BLAST?
TS PGECET - 2024
TS PGECET
Biotechnology
Bioinformatics and Genomics
For a given chamber pressure, the thrust of a rocket engine is highest when
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Rocket Propulsion
Which blotting technique is used for detection of proteins?
TS PGECET - 2024
TS PGECET
Biotechnology
Molecular Biology
The life of a geostationary communication satellite is limited by
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
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