An axisymmetric slender body comprising an ogive-cylinder (or ellipsoid -cylinder) shell enclosing an engine is analysed at various incidences to an incompressible uniform free stream for several jet flow rates on the basis of integral equation method.The pressure distributions, normal force, pitching moment, drag and thrust are calculated. The results with and without the effect of the exhaust jet flow are presented to show the influences of the jet mass flow rates on the aerodynamic properties.


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    Title :

    Numerical Solutions for Axisymmetric Bodies of Revolution Enclosing an Engine


    Additional title:

    Sae Technical Papers


    Contributors:
    Lin, M. H. (author) / Sheu, M. J. (author)

    Conference:

    Aerospace Technology Conference and Exposition ; 1990



    Publication date :

    1990-09-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English