Performance of external-compression bump inlet at Mach numbers of 1.5 and 2.0
Description:
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.
Date:
April 24, 1957
Creator:
Simon, Paul C.; Brown, Dennis W. & Huff, Ronald G.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department