A comparison of the aerodynamic characteristics at transonic speeds of four wing-fuselage configurations as determined from different test techniques
Description:
Report presenting a comparison of the high-speed aerodynamic characteristics of a family of four wing-fuselage configurations with four different degrees of sweepback as determined from transonic-bump model tests in the 7- by 10-foot tunnel, sting-supported model tests in the 8-foot tunnel, and the 7-foot by 10-foot tunnel.
Date:
October 4, 1950
Creator:
Donlan, Charles J.; Myers, Boyd C., II & Mattson, Axel T.
Item Type:
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Partner:
UNT Libraries Government Documents Department