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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design and experimental studies of low-cycle fatigue defects in turbine disks of aircraft long-life gas turbine engines


    Contributors:

    Published in:

    Publication date :

    2008-12-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Life prediction methodology for aircraft gas turbine engine disks

    MAHORTER, R. / LONDON, G. / FOWLER, S. et al. | AIAA | 1985


    Ceramic composite turbine disks for rocket engines

    Effinger, M.R. / Genge, G.G. / Kiser, J.D. | Tema Archive | 2000


    Aircraft gas turbine engines

    Engineering Index Backfile | 1948