Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Contributors:

    Conference:

    Joint propulsion conference



    Publication date :

    2015-01-01


    Size :

    17 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    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