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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Developments in STOL Aircraft Reported


    Publication date :

    1987


    Size :

    3 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Advanced Propeller Developments for V/STOL Aircraft

    Rosen, George | SAE Technical Papers | 1965


    Advanced propeller developments for V/STOL aircraft

    Rosen, G. | Engineering Index Backfile | 1965


    STOL aircraft

    MOMBRINIE BRUNO | European Patent Office | 2022

    Free access

    STOL AIRCRAFT

    MOMBRINIE BRUNO | European Patent Office | 2021

    Free access

    STOL AIRCRAFT

    MOMBRINIE BRUNO | European Patent Office | 2020

    Free access