The invention discloses a method for adjusting a wing class model and a system for adjusting the wing class model. The method for adjusting the wing class model comprises the steps that parameters are given to the wing class model, the wing class model is established, and the wing class model comprises N subsections; all the parameters influenced by the number of the sections of the wing class model are determined, and expressions between all the parameters and the N sections are generated; and the value of N in the wing class model is changed freely, and the numerical values of the parameters in the wing class model are adjusted correspondingly according to the expressions between all the parameters and the N sections, and accordingly the adjusted wing class model is established. According to the method for adjusting the wing class model, the expressions between all the parameters and the N sections are generated. Accordingly, the numerical values of the parameters in the wing class model are adjusted correspondingly according to the expressions between all the parameters and the N sections by freely changing the value of N in the wing class model, and thus the adjusted wing class model is established. Compared with the prior art, after the value of N is changed, the wing class model can be obtained without the need for establishing the model again.


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    Title :

    Method for adjusting wing class model and system for adjusting wing class model


    Contributors:
    HOU FEN (author) / LI JUNFU (author) / FU QING (author) / SHI JUANJUAN (author)

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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