Wing leading edge joint laminar flow tests /

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Bibliographic Details
Author / Creator:Drake, Aaron, author.
Imprint:Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, October 1996.
Description:1 online resource (33pages) : illustrations.
Language:English
Series:NASA technical memorandum ; 4762
NASA technical memorandum ; 4762.
Subject:
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/10757548
Hidden Bibliographic Details
Other authors / contributors:Ames Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Notes:Title from title screen (viewed Feb. 18, 2016).
"October 1996."
"Performing organization: Ames Research Center, Moffett Field, CA"--Report documentation page.
Includes bibliographical references (page 5).
Sponsored by the National Aeronautics and Space Administration 505-59-20 A-962704
Other form:Print version: Wing leading edge joint laminar flow tests
Microfiche version: Wing leading edge joint laminar flow tests
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:4762

MARC

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260 |a Moffett Field, California :  |b National Aeronautics and Space Administration, Ames Research Center,  |c October 1996. 
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490 1 |a NASA technical memorandum ;  |v 4762 
500 |a Title from title screen (viewed Feb. 18, 2016). 
500 |a "October 1996." 
500 |a "Performing organization: Ames Research Center, Moffett Field, CA"--Report documentation page. 
504 |a Includes bibliographical references (page 5). 
536 |a Sponsored by the National Aeronautics and Space Administration  |d 505-59-20  |d A-962704 
650 7 |a F-104 aircraft.  |2 nasat 
650 7 |a Laminar flow airfoils.  |2 nasat 
650 7 |a Friction measurement.  |2 nasat 
650 7 |a Skin friction.  |2 nasat 
650 7 |a Pressure distribution.  |2 nasat 
650 7 |a Laminar flow.  |2 fast  |0 http://id.worldcat.org/fast/fst00991079 
650 7 |a Skin friction (Aerodynamics)  |2 fast  |0 http://id.worldcat.org/fast/fst01120142 
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