Abstract Some data obtained in the course of numerous studies that include the calculated evaluation of the stressed state and cyclic life of disks up to low-cycle fatigue crack nucleation are presented. Also included are the extended investigations in metallurgy.
Design and experimental studies of low-cycle fatigue defects in turbine disks of aircraft long-life gas turbine engines
Russian Aeronautics (Iz VUZ) ; 51 , 4 ; 396-401
2008-12-01
6 pages
Article (Journal)
Electronic Resource
English
Ceramic composite turbine disks for rocket engines
Tema Archive | 2000
|Engineering Index Backfile | 1948