Numerical determination of the gas-dynamic behavior of vane cascades with various deflection angles of the trailing edges of longitudinal ribs of an advanced gas-turbine engine thrust reverser
Russian aeronautics ; 60 , 2
2017
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik | |
Lokalklassifikation TIB: | 770/7040/8000 |
Film Cooling of Insert Turbine Vane Trailing Edges
AIAA | 1972
|Aircraft engine thrust reverser
Emerald Group Publishing | 1998