The aerodynamic performance of a wing at an oblique deployment orientation has been found through wind tunnel testing to affect both the lateral and longitudinal stability of a cruise missile. While conventional analysis tools are insufficient for calculating the aerodynamics of an oblique wing, a suitable method has been determined for use with the USAF Missile DATCOM code. Comparisons made between wind tunnel results and Missile DATCOM calculations show that Missile DATCOM can produce a reasonable approximation of the aerodynamics of a wing at oblique deployment angles.


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    Titel :

    Oblique Wing Aerodynamics


    Beteiligte:
    M. A. McDaniel (Autor:in) / B. L. Wilks (Autor:in)

    Erscheinungsdatum :

    2004


    Format / Umfang :

    3 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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