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