Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Parametric Gas Turbine Modeling Approach for Assessing Transient Technologies in the Conceptual Design Phase (AIAA 2015-4030)


    Beteiligte:

    Kongress:

    Joint propulsion conference



    Erscheinungsdatum :

    01.01.2015


    Format / Umfang :

    17 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    A Parametric Gas Turbine Modeling Approach for Assessing Transient Technologies in the Conceptual Design Phase

    Ozcan, Metin F. / Perullo, Christopher / Tai, Jimmy C. et al. | AIAA | 2015


    Nr. 4030

    DataCite | 1922


    Simulation of a Canonical Shock Wave-Boundary Layer Interaction Using an LBM-VLES Approach (AIAA 2018-4030)

    Jammalamadaka, Avinash / Li, Yanbing / Gopalakrishnan, Pradeep et al. | British Library Conference Proceedings | 2018


    An Expert System-Driven Method for Parametric Trajectory Optimization During Conceptual Design (AIAA 2015-4486)

    Holt, James B. / Dees, Patrick D. / Diaz, Manuel J. et al. | British Library Conference Proceedings | 2015


    An Airport Assessment Approach in the Conceptual Design Stage (AIAA 2015-3185)

    Weiss, Marco / Dzikus, Niclas M. | British Library Conference Proceedings | 2015