This paper presents selected results of a panel loads study conducted as part of the final phase of an extensive investigation of an air-breathing missile concept employing wrap-around aerodynamic surfaces. Typical results for M = 2.36 are presented for the fin load results, plus a brief review of basic results of the previously reported tests. Vapor screen results are also discussed. The present results indicate that the fin load characteristics are nearly identical for planar and curved fins having the same projected planform and would permit the use of planar-surface predictions for supersonic speeds in the preliminary design stages of missiles employing wrap-around curved fins.


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    Titel :

    Control characteristics for wrap-around fins on cruise missiles configurations


    Beteiligte:
    Sawyer, W. C. (Autor:in) / Monta, W. J. (Autor:in) / Carter, W. V. (Autor:in) / Alexander, W. K. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1981 ; St. Louis, MO


    Erscheinungsdatum :

    01.01.1981


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Control Characteristics for Wrap-Around Fins on Cruise Missile Configurations

    W.C. Sawyer / W.J. Monta / W.V. Carter et al. | AIAA | 1982



    Techniques for roll tailoring for missiles with wrap-around fins

    DAHLKE, C. / DEEP, R. / OSKAY, V. | AIAA | 1983


    Non-linear Flight Dynamics of Unguided Missiles with Wrap-Around Fins

    Tannkulu, O. / Oenen, C. / Goekhan, T. et al. | British Library Conference Proceedings | 1998