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Problem 3 (20 p): As drawn in the figure, a static push rod will be designed to test a jet moter. The following conditions are given for a typical test: Intake air velocity = 200 m / s; exhaust gas velocity = 500 m / s; section area uptake = m, inlet static pressure = -22.5 kPa = 78.5 kPa (absolute pressure); input static temperature = 268 K; exhaust static pressure = 0 kPa = 101 kPa (absolute pressure). Find the minimum force Fa required for the design.

Control volume •Pam, -A P.1, PA Section (2) Section (1) F

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