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

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Bibliographic Details
Online Access: Online Access
Main Author: Jenkins, Renaldo V. (Author)
Corporate Author: Langley Research Center
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, May 1986.
Series:NASA technical paper ; 2565.
Subjects:

MARC

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264 1 |a Washington, D.C. :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c May 1986. 
300 |a 1 online resource (111 pages) :  |b illustrations. 
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490 1 |a NASA/TP ;  |v 2565 
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504 |a Includes bibliographical references (pages 9-10) 
513 |a Technical paper. 
588 |a Description based on online resource, PDF version; title from title page (NASA, viewed July 16, 2018) 
536 |a Langley Research Center  |d 505-61-01-02  |d L-16066. 
650 0 |a Aerofoils  |x Testing  |v Statistics. 
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650 0 |a Transonic wind tunnels.  |0 http://id.loc.gov/authorities/subjects/sh85136997 
650 0 |a Wall pressure (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85144916 
650 0 |a Boundary layer.  |0 http://id.loc.gov/authorities/subjects/sh85016095 
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