List of top Questions asked in TANCET

A closely coiled helical spring has a stiffness of 8N/mm. If it extends by 5 mm, the energy absorbed is
The physical principle used for the derivation of momentum equation is
The ratio of modulus of rigidity to bulk modulus for a Poisson's ratio of 0.25 would be:
The stress due to suddenly applied load is _______ compared to that of the gradually applied load?
The laminar flame speed in a combustion chamber of a jet engine is
What is the purpose of supercritical airfoil?
Which of the following assumptions / statements is NOT true about the Euler-Bernoulli beam theory?
Characteristic velocity of a rocket engine is equal to
Which of the following statements is true about Finite Element Analysis (FEA)?
Modified Tsai-Hill theory
Pressure gradient in the flow direction
Which type of grids is the best for flow over an airfoil?
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
Numerical panel methods are applicable for
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
The deflection of the free end of a cantilever beam subjected to a concentrated load at its mid span is given by:
In a turbojet engine, thrust specific fuel consumption ________ with increasing compressor pressure ratio and __________ with increasing turbine inlet temperature (within range of operation).
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
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 free stream Mach number for which the entire flow around the body is subsonic is called
The shape functions indicated here are for a
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
In the subcritical operation mode of a supersonic inlet, shock strands
A turbojet powered aircraft is suitable for which of the following type of applications?
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?