Abstract A computational technique, developed for analysis of strength, stability and low-cycle durability of GTE exhaust frame complex structure under operational and emergency loads is described. The presented technique, based on the ANSYS and STAR-CD engineering analysis software, and self-design software can improve the accuracy and efficiency of calculations, and reduce efforts on finite element mesh development, performing calculations and processing of results.
Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame
Russian Aeronautics (Iz VUZ) ; 54 , 4 ; 379-386
2011-12-01
8 pages
Article (Journal)
Electronic Resource
English
Computational analysis of strength, stability, and durability for gas turbine engine exhaust frame
Online Contents | 2011
|Turbine engine exhaust nozzle performance
AIAA | 1973
|The diesel-engine exhaust turbine
Engineering Index Backfile | 1928
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