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In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 / Robert D. Quinn and Leslie Gong.

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Format:
Book
Government document
Author/Creator:
Quinn, Robert D., author.
Gong, Leslie, author.
Contributor:
Hugh L. Dryden Flight Research Center
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Series:
NASA technical paper ; 1764.
NASA technical paper ; 1764
Language:
English
Subjects (All):
Turbulent boundary layer.
Heat--Transmission.
Heat.
Aerodynamic heating.
heat transmission.
Genre:
Online resources.
Physical Description:
1 online resource (49 pages) : illustrations
Place of Publication:
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980.
Notes:
Title from title screen (viewed on August 18, 2016).
"November1980."
"Performing Organization: NASA Dryden Flight Research Center"--Report documentation page
Includes bibliographical references (pages 18-19).
Electronic reproduction. [Place of publication not identified]: HathiTrust Digital Library. 2025.
Other Format:
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
OCLC:
760936051
Access Restriction:
Use copy Restrictions unspecified

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