This paper describes a test system of an 8% scale model of STOL aircraft 'ASKA' with turbine powered simulators tested at the Low Speed Wind Tunnel (6.5m) of National Aerospace Laboratory (NAL). The purpose of the system is to achieve high accurate measurements of aerodynamic forces by eliminating piping interferences. The paper also describes performance of the piping interference elimination function and overall system test results.


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    Title :

    Model with Turbine Powered Simulators at NAL's Low Speed Wind Tunnel Facility


    Publication date :

    2000


    Size :

    70 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English