Question: Consider one dimensional air isentropic flow through a duct . At a certain section of this duct.the velocity is 3 6 0 m / s
Consider one dimensional air isentropic flow through a duct At a certain section of this duct.the velocity is ms the temperature is deg C and the pressure is kPa. Find the Mach numberand the stagnation temperature and pressure at this point in the flow. If the temperature at some otherpoint in the flow deg C Find the Mach number and pressure at this point in the flow.
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