Inlet spillage drag tests and numerical flow-field analysis at subsonic and transonic speeds of a 1/8-scale, two-dimensional, external-compression, variable-geometry supersonic inlet configuration /
J.E. Hawkins, F.P. Kirkland, and R.L. Turner ; prepared by General Dynamics Convair Aerospace Division, Fort Worth. Tex., for Ames Research Center.

Description

Main Author

Hawkins, J. E.

Related Names

Turner, R. L. (Ralph Lilley), Sir, 1888-1983, joint author.
Kirkland, F. P., joint author.
Ames Research Center.
General Dynamics Corporation. Convair Aerospace Division.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington : U.S. National Aeronautics and Space Administration ; 1976.

Subjects

Jet engines > Jet engines / Air intakes.

Note

Cover title.

Physical Description

[1], 106 p. 3 folded p. of plates : ill. ; 27 cm.

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