Flight tests of a supersonic natural laminar flow airfoil /
Saved in:
Author / Creator: | Frederick, Michael A., author. |
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Imprint: | Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, December 2015. |
Description: | 1 online resource (29 pages) : illustrations. |
Language: | English |
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 |
Other authors / contributors: | NASA Neil A. Armstrong Flight Research Center, issuing body. |
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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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