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:Heat transfer coefficients.
Mach number.
Reynolds number.
Shear flow.
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