Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7
1957
43 pages
Report
No indication
English
Aerodynamics , Blunt body , Boundary layer transition , Cone , Turbulent heat transfer , Angle , Apex , Blunt , Body , Boundary , Flight , Flow , Heat transfer , Laminar , Layer , Sharp , Test , Transition , Turbulent