Nozzle wall boundary layers at Mach numbers 20 to 47
9th Aerospace Sciences Meeting ; 1971 ; New York , NY , U.S.A.
1971-01-01
Conference paper
Electronic Resource
English
Nozzle Wall Boundary Layers at Mach Numbers 20 to 47
| AIAA | 1972
Nozzle wall boundary layers at Mach numbers 20 to 47
| NTRS | 1971
Optical Characterization of Nozzle-Wall Mach-6 Boundary Layers (AIAA 2016-1586)
| British Library Conference Proceedings | 2016