The application of thrust augmentation concepts to short take-off and landing (STOL) aircraft propulsion is described for some typical installations. Aerodynamic and ejector thrust effects are treated separately so that the performance of the ejector-powered wing can be calculated as that of a jet-flapped airfoil and the ejector thrust components then added. Some considerations on the performance of the ejector-powered wing in cruise are included. A program for ejector calculations is given. (Author)


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    Title :

    Thrust Augmentation Considerations for STOL and Extended Cruise Propulsion


    Contributors:

    Publication date :

    1969


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English