NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Computational flowfields for static testing of powered hypersonic aftbody modelsTwo-dimensional CFD analyses are presented related to the ground testing of hypersonic, air-breathing models which feature scramjet exhaust flow simulation. CFD analysis indicates that it is possible to test aftbody powered hypersonic airbreather configurations in a static, pumped-down environment to obtain aftbody aerodynamic performance data.
Document ID
19930047955
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Huebner, Lawrence D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1993
Publication Information
Publication: Journal of Aircraft
Volume: 30
Issue: 1
ISSN: 0021-8669
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0021-8669
Accession Number
93A31952
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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