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    Titel :

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



    Kongress:

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



    Erscheinungsdatum :

    01.01.2005


    Format / Umfang :

    205 pages


    Anmerkungen:

    Includes bibliographical references and index; Papers on CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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    Hanus, D. / Censky, T. / Neveceral, J. et al. | British Library Conference Proceedings | 2005


    AIAA-2005-1056 STABILITY ANALYSIS OF A COMPRESSOR CASCADE

    Muhammad, M. / Fransson, T.H. / 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


    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


    Transonic/Supersonic Wind Tunnel Testing of the NASA Orion Command Module AIAA Paper

    Bell, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007