Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing
By: by M. D. Dobson.
Series: Aeronautical Research Council. Current papers, no. 1122; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 1122.
Publisher: H.M. Stationery Off.
Published: 1970
Place of publication: London
Language: eng
Number of pages: 22
Subjects: Cavities (Airplanes); Wind tunnels.
Notes: Includes bibliographical references.
Cover title.