Number of designs were previously developed around set of common design criteria; these designs used turboprop, fan-in-wing, and propulsive wing propulsion system arrangements; present report summarizes studies of performance of these aircraft when operated at off-design conditions and of design changes resulting from using different design criteria; some of basic aerodynamic input data that were utilized in developing these designs, and noise characteristics of some of designs, were evaluated.


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    Title :

    Additional studies on feasibility of V/STOL concepts for short-haul transport aircraft


    Additional title:

    NASA CR


    Contributors:
    Marsh, K.R. (author)

    Published in:

    Publication date :

    1967


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :