Q3solution - Description of Nozzle Flow Exit plane Mach...

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AAE 334 Fall 2011, Quiz #3 Name:___SOLUTIONS____ Compressible, steady, perfect-gas, quasi-one-dimensional flow of air in a converging- diverging nozzle. +1 point for correct answer, 0 for a blank, and -1 for wrong answer. Write the correct choice of <1, =1, of >1 in each shaded box.
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Unformatted text preview: Description of Nozzle Flow Exit plane Mach number BACK EXIT p p Subsonic flow throughout the nozzle <1 =1 Choked throat with subsonic flow in the diverging section <1 =1 Normal shock in the diverging section <1 =1 Over-expanded flow >1 <1 Under-expanded flow >1 >1...
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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.

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