NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
An experimental and analytical investigation of the aerodynamics of a hypersonic vehicle at free stream Mach 6The goal of this research is the assessment of the validity of existing three dimensional numerical programs in the prediction of the flow fields about general three dimensional hypersonic bodies. A detailed experimental research program was performed in which surface and flow field pressures were mapped. The results of the experimental work were compared with existing inviscid programs. Improvements were made on the existing numerical methods to include angle of attack. A summary of this work is presented.
Document ID
19810012497
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zakkay, V. (New York Univ. New York, NY, United States)
Wang, C. R. (New York Univ. New York, NY, United States)
Parikh, H. (New York Univ. New York, NY, United States)
Munakata, A. (New York Univ. New York, NY, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-164133
Accession Number
81N21026
Funding Number(s)
CONTRACT_GRANT: NSG-1444
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available