Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Information system and model for analyzing blade geometry and solving problems on ensuring quality of aircraft gas-turbine engines


    Contributors:


    Publication date :

    2016-01-01


    Size :

    6 pages



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Classification :

    DDC:    629.8 / 001.6




    BLADE STRUCTURE, AIRCRAFT BLADE, AND WIND TURBINE BLADE

    KIMURA SHIGEO / KOJIMA TETSUYA / ONOMA KEI | European Patent Office | 2016

    Free access

    Compressor-stall problems in gas-turbine type aircraft engines

    Benser, W.A. / Finger, H.B. | Engineering Index Backfile | 1956


    COMPRESSOR STALL PROBLEMS IN GAS-TURBINE-TYPE AIRCRAFT ENGINES

    Finger, Harold B. / Benser, William A. | SAE Technical Papers | 1957


    DIAGNOSTIC SYSTEM FOR AIRCRAFT TURBINE ENGINES

    Pintara, J. / Grupa projektowania antymeczeniowego konstrukcji | British Library Conference Proceedings | 2000