A study of low speed leading-edge flap design for supersonic cruise vehicle was conducted. Wings with flaps were analyzed with the aid of a newly developed subsonic wing program which provides estimates of attainable leading-edge thrust. Results indicate that the thrust actually attainable can have a significant influence on the design and that the resultant flaps can be smaller and simpler than those resulting from more conventional approaches.


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    Title :

    Application of an Aerodynamic Analysis Method Including Attainable Thrust Estimates to Low Speed Leading-Edge Flap Design for Supersonic Cruise Vehicles


    Contributors:

    Publication date :

    1982


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English