In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 /

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Bibliographic Details
Author / Creator:	Quinn, Robert D., author.
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980.
Description:	1 online resource (49 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1764 NASA technical paper ; 1764.
Subject:	Aerodynamic heating. Heat -- Transmission. Turbulent boundary layer.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10914238

Hidden Bibliographic Details
Other authors / contributors:	Gong, Leslie, author. Hugh L. Dryden Flight Research Center. United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Notes:	Title from title screen (viewed on Aug. 18, 2016). "November1980." "Performing Organization: NASA Dryden Flight Research Center"--Report documentation page. Includes bibliographical references (pages 18-19). Technical paper. National Aeronautics and Space Administration 505-43-24 H-1101
Other form:	Print version: Quinn, Robert D. In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 Microfiche version: Quinn, Robert D. In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1764

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