CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /
Saved in:
Author / Creator: | Davis, David O., author. |
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Imprint: | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015. |
Description: | 1 online resource (13 pages) : color illustrations. |
Language: | English |
Series: | NASA/TM ; 2015-218841 NASA technical memorandum ; 2015-218841. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10757944 |
Varying Form of Title: | Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction |
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Other authors / contributors: | NASA Glenn Research Center, issuing body. |
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). AJK2015-0634 |
GPO item no.: | 0830-D (online) |
Govt.docs classification: | NAS 1.15:2015-218841 |
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