Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    MULTIDISCIPLINARY OPTIMISATION OF HIGH PRESSURE TURBINE BLADE TIP WITH TURBINE INLET CAPACITY AND STAGE REACTION CONSTRAINTS


    Contributors:

    Conference:

    AIAA Aviation Forum ; 2021 ; Online



    Publication date :

    2021


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Multidisciplinary and Multiobjective Optimization Design of Long Blade Turbine Stage

    Li, B. / Song, L. / Li, J. et al. | British Library Online Contents | 2014



    Multidisciplinary optimization of gas turbine blade design

    Talya, Shashishekara / Rajadas, John / Chattopadhyay, Aditi | AIAA | 1998


    Multidisciplinary Optimization of Gas Turbine Blade Design

    Talya, S. S. / Rajadas, J. N. / Chattopadhyay, A. et al. | British Library Conference Proceedings | 1998