Cover Image

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

Bibliographic Details
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:
Airfoils.
Reynolds number.
Transonic wind tunnels.
Mach number.
Boundary layers.
Aerofoils > Testing > Statistics.
Wall pressure (Aerodynamics)
Boundary layer.
Aerofoils > Testing.
Statistics.
Online Access:https://purl.fdlp.gov/GPO/gpo105897

Internet

https://purl.fdlp.gov/GPO/gpo105897

Available Online

Holdings details from Available Online
Call Number: NAS 1.60:2565
 
Call Number Status Get It
NAS 1.60:2565 Available