R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
By: Renaldo V. Jenkins.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2565.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1986
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerofoils -- Testing -- Statistics.; Boundary layer.; Reynolds number.; Transonic wind tunnels.; Wall pressure (Aerodynamics); Airfoils.; Boundary layers.; Cryogenic wind tunnels.; Transonic wind tunnels.
Genres: Statistics.
Notes: Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1986. 2 microfiches.