PART 1

The maximum C1 that can be generated for a circulatory flow around a circular. Cylinder is. a. b. ... Flow aft of an oblique shock is supersonic where as aft of a normal shock it is subsonic. 1 .Explain the following in not more than 10 lines apart from sketches and plots; a. The diverging portion of a supersonic nozzle is always longer than ... ................
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