On the interaction of the transmitted shock with the boundary layer in a shock tube using argon as a test gas
By: by L. Davies and K. Bridgman.
Contributors: Bridgman, K., joint author.
Series: Aeronautical Research Council (Great Britain) Current papers,; no. 879; Current papers (Aeronautical Research Council (Great Britain)) ;; no. 879.
Publisher: H.M.S.O.
Published: 1967
Place of publication: London
Language: eng
Subjects: Shock tubes.; Shock waves.; Argon.; Boundary layer.
Notes: Bibliography: p. 9.
Cover title.