Experimental determination of pressure distributions on a plane wing with 40 degree sweepback at low speed
By: A. Martin M. Ingelmann-Sundberg.
Contributors: Royal Institute of Technology (Sweden). Division of Aeronautics
Series: Royal Institute of Technology. Division of Aeronautics. Technical note -- 8
Publisher: Royal Institute of Technology, Division of Aeronautics
Published: 1949
Place of publication: Stockholm
Number of pages: 20
Notes: Bibliographical references: p. 7.