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:	Aerofoils > Testing > Statistics. Reynolds number. Transonic wind tunnels. Wall pressure (Aerodynamics) Boundary layer. Airfoils. Mach number. Boundary layers. Aerofoils > Testing. Statistics.

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Call Number:	NAS 1.60:2565
NAS 1.60:2565	Available