Attached and Separated Boundary Layers on Highly Cooled, Ablating and Nonablating Models at M Equals 13.8
1967
66 pages
Report
Keine Angabe
Englisch
Aerodynamics , Boundary layer , Hypersonic flow , Separated flow , Ablation , Attachment , Blunt , Boundary , Conical , Cylinder , Flow , Geometry , Hemisphere , Hypersonic , Laminar , Layer , Model , Nose , Pressure , Reynolds number , Separation , Surface , Test , Transition