An analysis of the interaction of a boundary layer and the corner-expansion wave in supersonic flow
By: by P. H. Oosthuizen.
Series: UTIAS technical note ;; no. 117
Publisher: Institute for Aerospace Studies, University of Toronto]
Published: 1967
Place of publication: [Toronto
Language: eng
Subjects: Aerodynamics, Supersonic.; Boundary layer.; Laminar flow.; Turbulence.
Notes: Includes bibliographical references.
"AFOSR 67-1533."