Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system [microform] / J.R. DeBonis and C.J. Trefny.

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Bibliographic Details
Main Author:	DeBonis, James R.
Corporate Author:	NASA Glenn Research Center
Other Authors:	Trefny, Charles J.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2001]
Series:	NASA technical memorandum ; 210567.
Subjects:	Air breathing boosters. Hypersonic speed. Computational fluid dynamics. Wind tunnel tests. Propulsion. Pressure distribution.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:210567
NAS 1.15:210567	Restricted Place a Hold