Modes of failure found to be significant are considered which can be either aerodynamic, dynamic, structural, or combination of all 3; example of aero-thermal-elastic effects changing stability derivatives; when wing is exposed to loads and temperatures of selected flight profile, thermal deflections can be calculated using given temperature distribution; throughout mission profile, stability derivatives are changing and, thus, stability boundaries.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Modes of failure of hypersonic re-entry glide vehicle


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Fischler, J.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Entry Guidance with No-Fly Zone Avoidance for Hypersonic Glide Vehicle

    Zheng, Zonggui / Wang, Chongchong / Sun, Xiangdong et al. | British Library Conference Proceedings | 2022


    Entry Guidance with No-Fly Zone Avoidance for Hypersonic Glide Vehicle

    Zheng, Zonggui / Wang, Chongchong / Sun, Xiangdong et al. | TIBKAT | 2022


    Maneuver modes analysis for hypersonic glide vehicles

    Li, Guanghua / Zhang, Hongbo / Tang, Guojian et al. | IEEE | 2014


    Entry Guidance with No-Fly Zone Avoidance for Hypersonic Glide Vehicle

    Zheng, Zonggui / Wang, Chongchong / Sun, Xiangdong et al. | Springer Verlag | 2022