Experimental Investigation of Boundary-Layer Transition on a Cooled 7.5 Deg Total-Angle Cone at Mach 10
1967
37 pages
Report
Keine Angabe
Englisch
Aerodynamics , Fluid Mechanics , Boundary layer transition , Heat transfer , Hypersonic speed , Angle , Boundary , Cone , Distribution , Hypersonic , Layer , Reynolds number , Speed , Temperature , Theory , Transition , Wall