Question

The shock waves on a vehicle in supersonic flight cause a component of drag called supersonic wave drag define the wave drag coefficient as, where s is the suitable reference area for the body. In supersonic flight, the flow is governed in part by its thermodynamic properties, given by the specific heats at constant pressure and constant volume . Define the ratio using buckinghams pi theorem show that neglect the influence of friction.

Answer 1

HOPE IT HELPED YOU BRO

PLZ FOLLOW AND MARK ME BRAINLIEST ANSWER