Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes /

Bibliographic Details

Main Author:	Bobbitt, Percy J. (Author)
Format:	Government Document eBook
Language:	English
Published:	Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
Series:	NASA technical memorandum ; 2012-216004.
Subjects:	Supersonic flow. Wind tunnel tests. Wedges. Conical bodies. Conical flow. Cylindrical bodies. Orifices. Flight tests. Flow distribution.
Online Access:	https://purl.fdlp.gov/GPO/gpo37677