On the Flow Behind an Attached Curved Shock

• 1 November 1952
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
• Vol. 19  (11) , 734-742
• https://doi.org/10.2514/8.2457

Abstract

Keywords

• ATTACHED CURVED SHOCK
• FLOW BEHIND AN ATTACHED CURVED