Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Analysis of Anisotropy Effects for Transpiration Cooled CMC Leading Edges using OpenFOAM (AIAA 2015-3552)


    Beteiligte:

    Kongress:

    AIAA international space planes and hypersonic systems and technologies conference



    Erscheinungsdatum :

    01.01.2015


    Format / Umfang :

    14 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Analysis of Anisotropy Effects for Transpiration Cooled CMC Leading Edges using OpenFOAM

    Prokein, Daniel / Boehrk, Hannah / von Wolfersdorf, Jens | AIAA | 2015


    Nr. 3552

    DataCite | 1913


    Parametric Geometry Models for Hypersonic Aircraft Components: Blunt Leading Edges (AIAA 2015-3580)

    Kontogiannis, Konstantinos / Cerminara, Adriano / Taylor, Nigel J. et al. | British Library Conference Proceedings | 2015


    Gas Flow in a Generic Inlet with Blunted Leading Edges (AIAA 2015-1061)

    Radchenko, Vladimir / Borovoy, Volf / Mosharov, Vladimir et al. | British Library Conference Proceedings | 2015


    AIAA-2019-3552: Hydrofoil Conceptual Design and Optimization Framework for Amphibious Aircraft

    Seth, Arjit / Liem, Rhea P. | British Library Conference Proceedings | 2019