An investigation of boundary-layer transition on the wall of a Mach 5 nozzle. I - Disturbance measurements in a Mach 5 wind tunnel. II - Measurements and calculations of laminar, transitional, and turbulentboundary layers on the wall of a Mach 5 nozzle
12th Aerospace Sciences Meeting ; 1974 ; Washington , DC , U.S.A.
1974-01-01
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
AIAA | 1971
|