HW30 - Find the mass flow and momentum flow through this...

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AAE 334, Fall 2011 Homework 39 Due Friday, December 2, beginning of class. Air flows through a converging diverging nozzle in a steady flow. The air entering the nozzle has stagnation conditions psi p o 150 and R T o 500 . 1. The flow upstream of the throat is subsonic. At a certain axial position in the converging section of the nozzle, the Mach number is 0.3.
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Unformatted text preview: Find the mass flow and momentum flow through this cross section. 2. The throat is choked and at a cross section downstream of the throat, the area is 1.6 times the throat area. Find the mass flow and momentum flow through this cross section for: a. Subsonic flow b. Supersonic flow...
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This note was uploaded on 02/21/2012 for the course AAE 334 taught by Professor Collicott during the Fall '09 term at Purdue University-West Lafayette.

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