Experimental database with baseline CFD solutions : 2-D and axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions /
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| Author / Creator: | Marvin, Joseph G., author. |
|---|---|
| Imprint: | Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, November 2013. |
| Description: | 1 online resource (123 pages) : illustrations. |
| Language: | English |
| Series: | NASA/TM ; 2013-216604 NASA technical memorandum ; 2013-216604. |
| Subject: | Hypersonic shock. Turbulent boundary layer. Computational fluid dynamics. Two dimensional flow. Navier-Stokes equation. Hypersonic heat transfer. Computational fluid dynamics. Turbulent boundary layer. |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10297462 |