Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame
Russian aeronautics ; 54 , 4
2011
Article (Journal)
English
BKL: | 55.50 Luftfahrzeugtechnik | |
Local classification TIB: | 770/7040/8000 |
Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame
Springer Verlag | 2011
|Turbine engine exhaust nozzle performance
AIAA | 1973
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