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CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / David O. Davis.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Davis, David O., author.
- Series:
- NASA technical memorandum ; 2015-218841.
- NASA/TM ; 2015-218841
- Language:
- English
- Subjects (All):
- Computational fluid dynamics.
- Flow meters.
- Turbulence.
- flowmeters.
- Physical Description:
- 1 online resource (13 pages) : color illustrations.
- Other Title:
- Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
- Place of Publication:
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
- Notes:
- Title from title screen (viewed on Feb. 2, 2016).
- "September 2015."
- "Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015
- Includes bibliographical references (page 13).
- OCLC:
- 936387373
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