Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /

Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /

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Bibliographic Details
Author / Creator:Kegerise, Michael A., author.
Imprint:Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, November 2016.
Description:1 online resource (118 pages) : color illustrations.
Language:English
Series:NASA/TM ; 2016-219348
NASA technical memorandum ; 2016-219348.
Subject:
Reynolds number.
Wind tunnel models.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10994081
Hidden Bibliographic Details
Other authors / contributors:Neuhart, Dan H. (Dan Howard), 1952- author.
Langley Research Center, issuing body.
Notes:"November 2016."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (pages 30-31).
Technical memorandum.
Sponsored by the National Aeronautics and Space Administration 109492.02.07.01.01
L-20760
Description based on online resource; title from PDF title page (NASA, viewed Feb. 14, 2017).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2016-219348

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