R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /

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Bibliographic Details
Author / Creator:	Jenkins, Renaldo V., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, May 1986.
Description:	1 online resource (111 pages) : illustrations.
Language:	English
Series:	NASA/TP ; 2565 NASA technical paper ; 2565.
Subject:	Aerofoils -- Testing -- Statistics. Reynolds number. Transonic wind tunnels. Wall pressure (Aerodynamics) Boundary layer. Aerofoils -- Testing. Boundary layer. Reynolds number. Transonic wind tunnels. Wall pressure (Aerodynamics) Statistics.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/11665403

Hidden Bibliographic Details
Other authors / contributors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body. Langley Research Center.
Notes:	Prepared at Langley Research Center. "May 1986." Includes bibliographical references (pages 9-10). Technical paper. Langley Research Center 505-61-01-02 L-16066 Description based on online resource, PDF version; title from title page (NASA, viewed July 16, 2018).
Other form:	Print version: Jenkins, Renaldo V R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel Microfiche: Jenkins, Renaldo V R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:2565

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