Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /

Bibliographic Details
Main Authors:	DeBonis, James R. (Author), Trefny, Charles J. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
Series:	NASA technical memorandum ; 2001-210567.
Subjects:	Air breathing boosters. Hypersonic speed. Computational fluid dynamics. Wind tunnel tests. Propulsion. Pressure distribution.
Online Access:	https://purl.fdlp.gov/GPO/LPS23166

Description
Item Description:	"February 2001." "Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Physical Description:	1 online resource (18 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 5).