Title: Preliminary Data on the Effect of Body-nose Bluntness on the Drag and Pressure Recovery of a Side-inlet-body Combination at Mach Numbers of 1.4 and 1.7
Abstract: Memorandum presenting the pressure recovery, mass flow, and drag of a twin-scoop, side-inlet-body combination measured at Mach number 1.4 and 1.7. The inlet was located on a body having an ogival nose followed by a cylindrical section and a total fineness ratio of 5.
Publication Year: 1951
Publication Date: 1951-04-25
Language: en
Type: article
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