The influence of camber and geometrical twist on low-aspect-ratio wings of finite thickness in subsonic, transonic and supersonic flow
By: Friedrich Keune.
Contributors: Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical notes -- 29
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1953
Place of publication: Stockholm
Number of pages: 13
Notes: Bibliographical references: p. 13.