Wind tunnel tests for the Asuka were performed by using a transonic wind tunnel 2 x 2 m from late May to early June. The main purposes of the tests are as follows: to obtain basic aerodynamic data for expanding the flight area to the high-speed side at flight experiments on the Asuka; and to establish technologies necessary for performing tests on a power model in a transonic wind tunnel.


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    Titel :

    Developments in STOL Aircraft Reported


    Erscheinungsdatum :

    1987


    Format / Umfang :

    3 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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