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Author Quinn, Robert D., author.

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

Publication Info. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1764    ---  Available
Description 1 online resource (49 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical paper ; 1764
NASA technical paper ; 1764.
Note Title from title screen (viewed on Aug. 18, 2016).
"November1980."
"Performing Organization: NASA Dryden Flight Research Center"--Report documentation page.
Bibliography Includes bibliographical references (pages 18-19).
Type Of Report Technical paper.
Funding National Aeronautics and Space Administration 505-43-24
H-1101
Subject Turbulent boundary layer.
Heat -- Transmission.
Aerodynamic heating.
Aerodynamic heating. (OCoLC)fst00798175
Heat -- Transmission. (OCoLC)fst00953826
Turbulent boundary layer. (OCoLC)fst01159225
Heat transfer coefficients.
Mach number.
Reynolds number.
Shear flow.
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Gong, Leslie, author.
Hugh L. Dryden Flight Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form: Print version: Quinn, Robert D. In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 (OCoLC)7373501
Microfiche version: Quinn, Robert D. In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 (OCoLC)711544742
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.60:1764

 
    
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