Title: An experimental study of the lift and pressure distribution on a double-wedge profile at Mach numbers near shock attachment
Abstract: Report presenting an account of wind-tunnel measurements at low supersonic speeds of the pressure distribution on a doubly symmetrical double-wedge profile of approximately 8-percent thickness. The results cover a range of Mach numbers, angles of attack, and a specified Reynolds number. Results regarding the characteristics at zero angle of attack, characteristics at angle of attack, comparison with subsonic results, and some general remarks are provided.
Publication Year: 1954
Publication Date: 1954-07-01
Language: en
Type: article
Access and Citation
Cited By Count: 3
AI Researcher Chatbot
Get quick answers to your questions about the article from our AI researcher chatbot