An investigation was conducted to determine the low-speed flight dynamic behavior of a representative advanced turboprop business/commuter aircraft concept. Free-flight tests were conducted in the NASA Langley Research Center's 30- by 60-Foot Tunnel. In support of the free-flight tests, conventional static, dynamic, and free-to-roll oscillation tests were performed. Tests were intended to explore normal operating and post stall flight conditions, and conditions simulating the loss of power in one engine.


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    Title :

    Low-Speed Wind-Tunnel Investigation of the Flight Dynamic Characteristics of an Advanced Turboprop Business/Commuter Aircraft Configuration


    Contributors:
    P. L. Coe (author) / S. G. Turner (author) / D. B. Owens (author)

    Publication date :

    1990


    Size :

    50 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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