Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    High-Fidelity Aeroelastic Loads Calculation for a Transport Aircraft Configuration Including Pitch and Roll Maneuvers


    Beteiligte:

    Kongress:

    New results in numerical and experimental fluid mechanics (22nd symposium)



    Erscheinungsdatum :

    2021-01-01


    Format / Umfang :

    10 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    High-fidelity Aeroelastic Analysis of Very Flexible Aircraft

    Hallissy, B. / Cesnik, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011


    High-fidelity Aeroelastic Analysis of Very Flexible Aircraft

    Hallissy, Ben / Cesnik, Carlos | AIAA | 2011


    Minimum-time pitch maneuvers for combat aircraft

    Zweig, Avishay / Ben-Asher, Joseph | AIAA | 1995



    Aeroelastic effects on maneuvers: maneuver effects on aeroelastic stability

    Olsen, J. J. | British Library Conference Proceedings | 1993