A low noise STOL experimental aircraft, Asuka, is presently being researched and developed at a full scale flight experimental stage. The main wing itself of the C-1 transport, which is the mother aircraft of the Asuka, was not changed because the main purpose of this research was to establish a upper surface blowing which will realize a revolutionary STOL performance. Research has also been conducted on the possibility of a rise in aerodynamic performance of the optimum shape of main wings as part of the research on the practical use of future STOL aircraft. Tests were conducted in the above research by using a half-cut model with a main wing shape designed with a computer aided design system and are called low speed wind tunnel test.


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    Title :

    CAD (Computer Aided Design) Wind Tunnel Test for Half-Cut Model of Asuka


    Publication date :

    1987


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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