Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Description:
From Introduction: "The results obtained in the wind-tunnel tests at Mach numbers 2.36 and 2.87 for several configurations utilizing this wing, including results on the wing alone are presented."
Date:
August 4, 1958
Creator:
Hallissy, Joseph M., Jr. & Hasson, Dennis F.
Item Type:
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Partner:
UNT Libraries Government Documents Department