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Hypersonic nozzle/afterbody CFD code validation. I - Experimental measurementsThis study was conducted to obtain a detailed experimental description of the flow field created by the interaction of a single-expansion-ramp-nozzle flow with a hypersonic external stream. Data were obtained from a generic nozzle/afterbody model in the 3.5-Foot Hypersonic Wind Tunnel of the NASA Ames Research Center in a cooperative experimental program involving Ames and the McDonnell Douglas Research Laboratories. This paper presents experimental results consisting primarily of surveys obtained with a five-hole total-pressure/flow-direction probe and a total-temperature probe. These surveys were obtained in the flow field created by the interaction between the underexpanded jet plume and the external flow.
Document ID
19930040734
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spaid, Frank W.
(McDonnell Douglas Corp. Saint Louis, MO, United States)
Keener, Earl R.
(Eloret Inst. Palo Alto, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 93-0607
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A24731
Funding Number(s)
CONTRACT_GRANT: NCC2-553
Distribution Limits
Public
Copyright
Other

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