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    Titel :

    AIAA-2005-1221 FIRST STAGE OF THE CENTRIFUGAL COMPRESSOR DESIGN WITH TANDEM ROTOR BLADES



    Kongress:

    17th, International symposium on air breathing engines ; 2005 ; Munich, Germany



    Erscheinungsdatum :

    01.01.2005


    Format / Umfang :

    187 pages


    Anmerkungen:

    Includes bibliographical references and index; Papers on CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    AIAA-2005-1222 TWO-STAGE SINGLE-SHAFT CENTRIFUGAL COMPRESSOR ADVANCED DESIGN

    Matousek, O. / Neveceral, J. / Hanus, D. et al. | British Library Conference Proceedings | 2005


    AIAA-2005-1058 BOUNDARY LAYER DEVELOPMENT ON ROTOR BLADES OF A FOUR-STAGE LOW-SPEED AXIAL COMPRESSOR

    Muller, L. / Mailach, R. / Vogeler, K. et al. | British Library Conference Proceedings | 2005


    AIAA-2005-1242 TESTING DETERIORATION OF COMPRESSOR FIRST STAGE BLADES IN SUPERSONIC CASCADE WIND TUNNEL

    Tabakoff, W.P.J. / Mason, R. / American Institute of Aeronautics and Astronautics; International Society for Air Breathing Engines | British Library Conference Proceedings | 2005


    AIAA-2005-1182 A 3D HYBRID DESIGN METHOD OF COMPRESSOR BLADES

    Ugryumov, M.L. / Tsegelnik, A.M. / Menyaylov, A.V. et al. | British Library Conference Proceedings | 2005


    Nr. 1221

    DataCite | 1868

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