Question: 4 . 7 A turbojet engine under static test ) = ( 0 has air with a mass flow of 1 0 0 k g

4.7 A turbojet engine under static test )=(0 has air with a mass flow of 100kgs flowing through an inlet area A1 of 0.56m2 with a total pressure of 1 atm and total temperature of 288.8 K . Determine the additive drag of the inlet.
4 . 7 A turbojet engine under static test ) = ( 0

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