Slender‐body theory is used to calculate the effects on the lift and moment of mounting the wing of a wing‐body combination above or below the body axis. The effects of the asymmetrical mounting can become substantial when the body diameter is more than half of the wing span. These effects will fall off as the body shrinks. This theory is particularly useful in the aerodynamic design considerations pertinent to the performance of slender‐body vehicles operating at high velocities and high altitudes. The lift and drag forces acting on a slender‐body vehicle strongly depend on the relative effects of leading‐edge bluntness and boundary layer displacement. Ballistic missile is a typical slender‐body vehicle meant for operation under extreme heat transfer condition for a few seconds. In most cases, the maximum heating rates can be calculated using blunt body stagnation point theories developed for the ballistic missiles.


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    Titel :

    Application of Slender‐body Theory


    Beteiligte:


    Erscheinungsdatum :

    31.03.2025


    Format / Umfang :

    21 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Application of slender-body theory

    Kaplan, P. | Engineering Index Backfile | 1957


    Slender-body theory -- Review and extension

    Adams, M.C. / Sears, W.R. | Engineering Index Backfile | 1953


    On slender-body theory at transonic speeds

    Harder, Keith C / Klunker, E B | NTRS | 1954



    On slender-body theory at transonic speeds

    Harder, Keith C. / Klunker, E. B. | TIBKAT | 1957