Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By: William G. Johnson and Acquilla S. Hill.
Contributors: Hill, Acquilla S.; United States. National Aeronautics and Space Administration.
Publisher: NASA
Published: 1985
Place of publication: Washington
Number of pages: 266
Subjects: Airfoils