The invention is in the field of configuring the shape or geometry of an aircraft airfoil. In particular, the present invention provides a method for designing an exterior geometry of an aircraft airfoil.

    本发明属于配置飞行器翼型的形状或几何结构的领域。特别地,本发明提供了一种用于设计飞行器翼型的外部几何结构的方法。


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    Title :

    Simplified method of parametric surface generation


    Additional title:

    参数表面生成的简化方法


    Contributors:

    Publication date :

    2023-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    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 / B64C AEROPLANES , Flugzeuge



    SIMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION

    LLAMAS SANDIN RAÚL CARLOS / BAILEY NOVAL NICOLÁS | European Patent Office | 2023

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    SIMPLIFIED METHOD FOR PARAMETRIC SURFACE GENERATION

    LLAMAS SANDIN RAUL CARLOS / BAILEY NOVAL NICOLAS | European Patent Office | 2023

    Free access

    Strategies To Design Simplified, Parametric Body Structures

    Boehme, M. / Haenschke, A. / Appel, H. | British Library Conference Proceedings | 1997


    Simplified model for predicting the onset of parametric rolling

    Surendran, S. / Lee, S.K. / Sohn, K.H. | Tema Archive | 2007


    Surface and Volume Grid Generation in Parametric Form

    Yu, T. / Soni, B. K. / Benjamin, T. et al. | British Library Conference Proceedings | 1996