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The pressure-recovery characteristics at the vertical center line of an NACA submerged inlet of aspect ratio 5 have been measured in the Mach number range 0.60
Language: en
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Type: BOOK - Published: 1992 - Publisher:
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Type: BOOK - Published: 2018-07-17 - Publisher: Createspace Independent Publishing Platform
A flow-through inlet test program was conducted to evaluate inlet test methods and determine the impact of the fan on inlet separation when operating at large a