Investigations on a STOL aircraft with internally blown flaps are described. To avoid separation on the wing, slots were located behind the nose flap and in front of the trailing edge flap. The investigations were designed to examine maximum lift and lift/drag ratio. In addition, the effectiveness of the aileron and the horizontal tail were investigated. (Author)


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    Title :

    Three-Component Measurements on a Model of a Light STOL Aircraft with Chordwise Blowing


    Contributors:
    H. Koerner (author)

    Publication date :

    1976


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English