Title: Pressure-distribution and ram-recovery characteristics of NACA submerged inlets at high subsonic speeds
Abstract: Report presenting ram-recovery and mass-flow ratios for submerged inlets at four positions on the fuselage of a model of a hypothetical fighter airplane. Results related to the inlet location and effect of angle of attack are also provided.
Publication Year: 1950
Publication Date: 1950-07-07
Language: en
Type: article
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Cited By Count: 5
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