Analysis of Hypersonic Pressure and Heat Transfer Tests on a Flat Plate with a Flap and a delta Wing with Body, Elevons, Fins, and Rudders Final Report
1966
126 pages
Report
No indication
English
Aerodynamics , Flow field , Hypersonic boundary layer , Body , Boundary , Delta , Elevon , Field , Fin , Flap , Flat , Flow , Heat transfer , Interference , Layer , Plate , Separation , Testing , Wing , X- 20 aircraft
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