Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers from 1.90 to 3.07
1958-03-24
Miscellaneous
No indication
English
Transition on swept leading edges at Mach 3.5
NTRS | 1987
|Transition on swept leading edges at Mach 3.5
AIAA | 1987
|Leading Edge Transition on a 76 Degree Swept Cylinder at Mach 1.6
British Library Conference Proceedings | 1996
|