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    Titel :

    AIAA-2005-1113 BALLISTIC COOLING OF TURBINE NOZZLE GUIDE VANE PLATFORMS



    Kongress:

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



    Erscheinungsdatum :

    2005-01-01


    Format / Umfang :

    90 pages


    Anmerkungen:

    Includes bibliographical references and index; Papers on CD-ROM



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    AIAA-2005-1118 NUMERICAL AND EXPERIMENTAL INVESTIGATIONS OF NOZZLE GUIDE VANE ENDWALL HEAT TRANSFER

    Rubensdorffer, F.G. / Fransson, T.H. / American Institute of Aeronautics and Astronautics; International Society for Air Breathing Engines | British Library Conference Proceedings | 2005


    AIAA-2007-1162 SENSITIVITY ANALYSIS FOR HIGH PRESSURE TURBINE NOZZLE GUIDE VANE TEMPERATURE PREDICTION

    Ravitej, M. / Kesavan, V. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007


    An Investigation of Twin Supersonic Jet Coupling (AIAA 2016-1113)

    Kuo, Ching-Wen / Cluts, Jordan D. / Samimy, Mo | British Library Conference Proceedings | 2016


    Nr. 1113

    DataCite | 1866

    Freier Zugriff

    Nr. 1113

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