List of top Aeronautical and Aerospace Engineering Questions

The shape functions indicated here are for a
Axisymmetric problems involving axisymmetric loading and solids of revolution can be conveniently formulated with the following element type.
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:
Modified Tsai-Hill theory
A closely coiled helical spring has a stiffness of 8N/mm. If it extends by 5 mm, the energy absorbed is
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
The ratio of modulus of rigidity to bulk modulus for a Poisson's ratio of 0.25 would be:
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:
In a short column with eccentric loading, the neutral axis: