Transonic wind-tunnel tests of an F-8 airplane model equipped with 12- and 14- percent thick oblique wings
By: Ronald C. Smith, Robert T. Jonesand James L. Summers.
Contributors: Jones, Robert T. 1910-; Summers, James L.
Series: Technical memoranda / National Aeronautics and Space Administration -- TM-X-62478
Publisher: NASA Ames Research Center
Published: 1975
Place of publication: Moffett Field, California
Language: eng