Large Eddy Simulation of a film cooling flow injected from an inclined discrete cylindrical hole into a crossflow with zero-pressure gradient turbulent boundary layer /
Saved in:
Author / Creator: | Johnson, Perry L., author. |
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Imprint: | Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012. |
Description: | 1 online resource (23 pages) : color illustrations. |
Language: | English |
Series: | NASA/TM ; 2012-217695 NASA technical memorandum ; 2012-217695. |
Subject: | Large eddy simulation. Film cooling. Pressure gradients. Reynolds averaging. Turbulent mixing. Turbulent boundary layer. Turbulent boundary layer. |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/8951880 |
Other authors / contributors: | Shyam, Vikram, author. NASA Glenn Research Center. |
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Notes: | Title from title screen (viewed on Dec. 26, 2012). "August 2012." Includes bibliographical references (pages 22-23). Sponsored by National Aeronautics and Space Administration NNC097A01C WBS 561581.02.08.03.21.14.03 E-18382 |
GPO item no.: | 0830-D (online) |
Govt.docs classification: | NAS 1.15:2012-217695 |
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