Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /
William G. Johnson, Jr., and Acquilla S. Hill.

Description

Main Author

Johnson, William G. (William Garland), 1944-

Related Names

Hill, Acquilla S.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.

Subjects

Transonic wind tunnels.
Low temperature research.
Reynolds number.
Aerodynamics, Transonic.
Aerofoils > Aerofoils / Testing > Aerofoils / Testing / Statistics.

Note

Prepared at Langley Research Center.
Chiefly graphs and tables.

Physical Description

iii, 266 p. : ill. ; 28 cm.

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