Flight tests of a supersonic natural laminar flow airfoil /

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Bibliographic Details
Author / Creator:Frederick, Michael A., author.
Imprint:Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, December 2015.
Description:1 online resource (29 pages) : illustrations.
Series:NASA/TM ; 2015-218940
NASA technical memorandum ; 2015-218940.
Subject:Boundary layer transition.
Chords (geometry)
Laminar flow.
Leading edge sweep.
Supersonic airfoils.
Laminar flow.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10759710
Hidden Bibliographic Details
Other authors / contributors:NASA Neil A. Armstrong Flight Research Center, issuing body.
Notes:Title from title screen (viewed April 20, 2016).
"December 2015."
Includes bibliographical references (page 29).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2015-218940

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