A finite-difference method for predicting supersonic turbulent boundary-layer flows with tangential slot injection
NASA contractor report ; CR-2124
1972
XII, 68 S
graph. Darst
Contract or grant no. NGR-47-004-072
Report
Englisch
Tangential slot injection in supersonic flow
AIAA | 1967
|Tangential slot injection in supersonic flow.
AIAA | 1967
|