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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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- Fall '09