The influence of shock and boundary layer interaction on shock tube flows
By: by L. Davies and J.L. Wilson.
Contributors: Wilson, J. L.; National Physical Laboratory. Aerodynamics Division.
Series: NPL Aero report -- 1228; ARC 29 064; Hyp. 615
Publisher: National Physical Laboratory
Published: 1967
Place of publication: [Teddington]
Language: eng