Effects of suction on the interaction between shock wave and boundary layer at a compression corner
By: by L. H. Tanner and S. L. Gai.
Contributors: Gai, S. L., joint author.
Series: Aeronautical Research Council. Current papers, no. 1087; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 1087.
Publisher: H.M. Stationery Off.
Published: 1970
Place of publication: London
Language: eng
Number of pages: 16
Subjects: Aerodynamics, Supersonic.; Shock waves.; Boundary layer.
Notes: Bibliography: p. [1] (2nd group)
Cover title.