Report describes observations of supersonic flow of air over cylindrical body capped by hemisphere at its head and flared to cone at its tail end. Study prompted by need for greater aircraft control at high angles of attack.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flow Over A Simplified-Rocket-Shaped Body


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1992-02-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rocket body turning-over device and rocket hoisting system

    PENG XIAOBO / DONG YANMIN / LI JINMEI | Europäisches Patentamt | 2020

    Freier Zugriff

    On Simplified Mechanical Models for Rocket-Body Divergence and Flutter

    Ohshima, Tsukasa / Sugiyama, Yoshihiko | AIAA | 2003


    On Simplified Mechanical Models for Rocket-Body Divergence and Flutter

    Ohshima, T. / Sugiyama, Y. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    SIMPLIFIED SHUTTLE MODULE FOR CARRIER ROCKET

    PRAMPOLINI MARKO | Europäisches Patentamt | 2015

    Freier Zugriff

    Ring-shaped booster rocket

    STARKEY RYAN / ALTAMIRANO DARIO N | Europäisches Patentamt | 2023

    Freier Zugriff