An approximate method for the determination of the increase of maximum lift on thin profiles due to trailing edge flaps
By: H. O. Palme and S. Stark.
Contributors: Stark, S.; Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical note -- 18
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1950
Place of publication: Stockholm
Notes: Bibliography: p. 6.