Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream
By: by J. A. Lawford.
Series: Aeronautical Research Council. Current papers,; no. 1108; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 1108.
Publisher: H. M. Stationery Off.
Published: 1970
Place of publication: London
Language: eng
Number of pages: 35
Subjects: Wind tunnels.; Aerodynamics.
Notes: Includes bibliographical references.
Cover title.