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A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel
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Published Year
1950-1959 (1)
Subject
Aerodynamics, Supersonic (1)
Airplanes--Fuselage (1) *
Supersonic planes (1)
Author
Hasel, Lowell E. (1) *
Sinclair, Archibald R. (1)
