Development of an axisymmetric afterbody test case for turbulent flow separation validation /

Development of an axisymmetric afterbody test case for turbulent flow separation validation /

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Bibliographic Details
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
Hidden Bibliographic Details
Other authors / contributors:Rumsey, C. L. (Christopher Lockwood), 1961- author.
Langley Research Center, issuing body.
Notes:"November 2017."
Includes bibliographical references (pages 26-27).
Technical memorandum.
Sponsored by National Aeronautics and Space Administration 109492.02.07.01.01
Description based on online resource, PDF version; title from title page (NASA, viewed Dec. 15, 2017).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2017-219680

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