Investigation of an Underslung Normal-Wedge Inlet at Free-Stream Mach Numbers From 1.50 to 1.99
Description:
Wedge and scoop air inlet performance and thrust minus drag comparisons at free stream in supersonic wind tunnel test.
Date:
March 19, 1957
Creator:
Vargo, Donald J. & Weinstein, Maynard I.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department