Title: Performance of external-compression bump inlet at Mach numbers of 1.5 and 2.0
Abstract: Report presenting an experimental investigation of a scale model of the forebody of a proposed supersonic fighter to determine the internal performance and configuration drag of various twin-side inlets. External-compression ramp and bump inlets with various types and combinations of boundary-layer bleed were tested. Results regarding performance charts and flow characteristics are provided.
Publication Year: 1957
Publication Date: 1957-04-24
Language: en
Type: article
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Cited By Count: 15
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