TORSIONAL STRESS Shear stress produced when we apply the twisting moment to the end of a shaft about its axis is known as Torsional stress.
The velocity, relative to a rocket at which exhaust gases leave the nozzle of the rocket's engine.
It is an analytical expression directly related to the size of the adverse pressure gradient to be encountered by the boundary layer
The nozzle contribution to engine thrust is called gross thrust. It comprises two terms, namely, the momentum thrust and the pressure thrust
The inlet area at the lip, which is also known as the highlight, is called the inlet capture area and is sometimes given the symbol Ac. The capture (area) ratio…