Analysis of angle-of-attack history of spinning body; asymptotic solution for resultant angle-of-attack is derived, applicable to any axially symmetric body having aerodynamic restoring-moment coefficient proportional to sine of resultant angle-of-attack; solution yields results in satisfactory agreement with results obtained from numerical integrations of exact equations of motion.


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    Titel :

    Angle-of-attack convergence of spinning bodies entering planetary atmospheres at large inclinations to flight path


    Weitere Titelangaben:

    NASA -- Tech Report


    Beteiligte:
    Tobak, M. (Autor:in) / Peterson, V.L. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :