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 /
by Lowell E. Hasel and Archibald R. Sinclair

Description

Main Author

Hasel, Lowell E.

Related Names

Sinclair, Archibald R.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1950.

Subjects

Aerodynamics, Supersonic.
Supersonic planes.
Airplanes > Airplanes / Fuselage.

Note

"April 7, 1950; Declassified May 29, 1959."

Physical Description

49 p. : ill. ; 27 cm.

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