Effect of geometric dihedral on low-speed static stability characteristics of a 40 degree swept-back wing
By: Kazimierz Orlik-Ruckemann.
Contributors: Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical note -- 17
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1950
Place of publication: Stockholm
Number of pages: 18
Notes: Bibliographical references: p. 8.