approximate method of calculating the subsonic velocity distribution on high-aspect-ratio swept wings of small thickness at zero lift
By: Friedrich Keune.
Contributors: Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical notes -- 26
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1953
Place of publication: Stockholm
Number of pages: 36
Notes: Bibliographical references: p. 32.