List of top Questions asked in TANCET

Consider an equal-leg angle section cantilever beam subject to a vertical shearing load at the tip where the line of action of the applied vertical force passes through the centroid. This beam will experience
Numerical panel methods are applicable for
Pressure gradient in the flow direction
Consider an infinitely thin flat plate at an angle of attack of \(5^\circ\) in a Mach 2.3 flow. Pressure is 101 kPa. The lift coefficient as per shock expansion theory is
A rectangular section beam subjected to a bending moment M varying along its length is required to develop the same maximum bending stress at any cross section. If the depth of the section is constant, then its width will vary as:
The semi-span of a rectangular wing of plan form area 8.4 m² is 3.5 m. The aspect ratio of the wing is
The lifting flow over circular cylinder is obtained by the combination of
When a nozzle is said to be over expanded?
The physical principle used for the derivation of momentum equation is
The function \( y = A \left(1 - \cos\left(\frac{2\pi x}{L}\right)\right) \) is an allowed approximate function for a
Which of these analyses needs a stretched grid?
The combustion in a gas turbine is a
The stress due to suddenly applied load is _______ compared to that of the gradually applied load?
The concept of erosive burning in solid rocket propellant operation pertains to
Which of the following statements is true about Finite Element Analysis (FEA)?
Ram efficiency is defined as
What is the purpose of a fuel injection system in the combustor?
For a given rotational speed of a rotor of an axial flow compressor, as the fan tip radius increases, the centrifugal stress on the fan blade
If two shafts of same length, one of which is hollow, transmit equal torque and have equal maximum shear stress, then they should have equal
In a short column with eccentric loading, the neutral axis:
If a laminate consists of pairs of layers with identical thickness and elastic properties, but with orientation of +θ and -θ with respect to the laminate reference axis, then the laminate is called as
AB = 40 cm while BC = 30 cm. Areas A and C are equal to 8 \( \text{cm}^2 \) while areas B and D are 6 \( \text{cm}^2 \). The given section is subject to \( M_x = 100 \text{kNm} \) and \( M_y = 40 \text{kNm} \). Find an expression for the bending stress. Assume that the webs are ineffective in bending.
For isentropic flows the value of work-done factor for a turbo machine (\(\Psi\)) will be
Specific impulse of a rocket
What is the center pressure if the lift coefficient and lift curve slope of an aerofoil of percentage camber 0.6 are 1.02 and 2, respectively?