Nozzle boundary-layer displacement thickness at Mach numbers 30 to 70
MILLER, C. G. /NASA, LANGLEY RESEARCH CENTER, AERO-PHYSICS DIV., HAMPTON, VA./.
AIAA Journal ; 7 , 11 ; 2165-2167
1969-01-01
3 pages
Article (Journal)
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
|