Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semicircular Air Inlet in the Root of a 45 Degree Sweptback Wing
Description:
Report presenting an investigation in the transonic blowdown tunnel at Mach numbers from 0.63 to 1.41 to determine increments in lift, drag, and pitching moment of a sweptback semicircular air inlet installed in the root of a 45 degree sweptback wing. Results regarding internal pressures and inlet performances are provided.
Date:
March 23, 1955
Creator:
Trescot, Charles D., Jr. & Keith, Arvid L., Jr.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department