The students get an understanding of nature of flow past various models through flow visualization techniques. The nature of pressure distribution over various aerofoil and body shapes is explained. The wake and boundary layer survey provide information on the momentum thickness and displacement thickness.
Experiments related to aircraft engines, force measurements through wall jets and measurement of speed of flame propagation is checked.
It provides the student with the practical knowledge of the various theorems, like reciprocal theorem, buckling phenomenon of columns, WAGNER beam stresses information. The vibration of beam equipment provides information on types of nodes and vibration patterns.
it helps the students to get the practical knowledge in engine, compressor & subsystems of engines.