Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model /
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| Author / Creator: | Kim, S. W. |
|---|---|
| Imprint: | [Washington, D.C.] : [National Aeronautics and Space Administration] ; [Springfield, Va. :] : [For sale by the National Technical Information Service], [1990] |
| Description: | 38 pages : illustrations. |
| Language: | English |
| Series: | NASA technical memorandum ; 102499 NASA technical memorandum ; 102499. |
| Subject: | Turbulence. Compressible flow. Separated flow. Shock wave interaction. Transonic flow. Turbulence models. Turbulent boundary layer. Turbulent flow. |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/6504683 |
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| 100 | 1 | |a Kim, S. W. |0 http://id.loc.gov/authorities/names/n98082332 |1 http://viaf.org/viaf/75634199 | |
| 245 | 1 | 0 | |a Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model / |c S.W. Kim. |
| 264 | 1 | |a [Washington, D.C.] : |b [National Aeronautics and Space Administration] ; |a [Springfield, Va. :] : |b [For sale by the National Technical Information Service], |c [1990] | |
| 300 | |a 38 pages : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a microform |b h |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/h | ||
| 338 | |a microfiche |b he |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/he | ||
| 490 | 1 | |a NASA technical memorandum ; |v 102499 | |
| 500 | |a Cover title. | ||
| 500 | |a "Institute for Computational Mechanics in Propulsion." | ||
| 500 | |a "January 1990." | ||
| 500 | |a "ICOMP-90-04." | ||
| 504 | |a Includes bibliographical references (pages 28-31). | ||
| 538 | |a Available via Internet from the NASA Technical Report Server web site. Address as of 8/4/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012646%5F1990012646.pdf ; current access is available via PURL | ||
| 650 | 0 | |a Turbulence. |0 http://id.loc.gov/authorities/subjects/sh85138753 | |
| 650 | 7 | |a Compressible flow. |2 nasat | |
| 650 | 7 | |a Separated flow. |2 nasat | |
| 650 | 7 | |a Shock wave interaction. |2 nasat | |
| 650 | 7 | |a Transonic flow. |2 nasat | |
| 650 | 7 | |a Turbulence models. |2 nasat | |
| 650 | 7 | |a Turbulent boundary layer. |2 nasat | |
| 650 | 7 | |a Turbulent flow. |2 nasat | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 710 | 2 | |a Lewis Research Center. |b Institute for Computational Mechanics in Propulsion. |0 http://id.loc.gov/authorities/names/n93005993 |1 http://viaf.org/viaf/154916464 | |
| 830 | 0 | |a NASA technical memorandum ; |v 102499. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/LPS62525 |y Government Publishing Office |
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