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
By: J. E. Hawkins, F. P. Kirkland, and R. L. Turner ; prepared by General Dynamics Convair Aerospace Division, Fort Worth. Tex., for Ames Research Center.
Contributors: Kirkland, F. P.; Turner, R. L. Sir, 1888-; United States. National Aeronautics and Space Administration.; General Dynamics Corporation. Convair Division.; Ames Research Center.
Series: NASA contractor report ; NASA CR-2680; NASA contractor report -- NASA CR-2680.
Publisher: U.S. National Aeronautics and Space Administration; for sale by the National Technical Information Service
Published: 1976
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 106
Subjects: Airplanes -- Jet propulsion -- Air intakes.
Notes: Cover title.

Bibliography: p. 46.