Development of an axisymmetric afterbody test case for turbulent flow separation validation / 2017-219680
Saved in:
| Author / Creator: | Disotell, Kevin J., author. |
|---|---|
| Imprint: | Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, November 2017. |
| Description: | 1 online resource (iv, 27 pages) : color illustrations. |
| Language: | English |
| Series: | NASA/TM ; 2017-219680 NASA technical memorandum ; 2017-219680. |
| Subject: | Turbulence models. Computational fluid dynamics. Afterbodies. Boundary layer separation. Separated flow. |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/11555095 |