The aerodynamic performance of a certain aircraft wing structure at different angles of attack was analyzed using FLUENT finite element software. According to simulation, the lower surface of the wing is a high-pressure zone, while the upper surface is a low-pressure zone. As the angle of attack increases, the high-pressure zone will move towards the leading edge of the wing, while the trailing edge of the wing slowly forms a low-pressure zone; At the same time, the airflow accelerates on the surface of the wing, causing a decrease in pressure and an increase in lift. This provides a theoretical basis for further optimizing the wing structure.


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    Titel :

    Analysis of aerodynamic characteristics of a certain aircraft wing structure at different angles of attack


    Beteiligte:
    Pan, Lijia (Herausgeber:in) / Zhou, Zaifa (Herausgeber:in) / Hu, Shushan (Autor:in) / Yin, Zedong (Autor:in) / Liu, Ronge (Autor:in)

    Kongress:

    Ninth International Symposium on Sensors, Mechatronics, and Automation System (ISSMAS 2023) ; 2023 ; Nanjing, China


    Erschienen in:

    Proc. SPIE ; 12981


    Erscheinungsdatum :

    2024-03-04





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Wing-Alone Aerodynamic Characteristics at High Angles of Attack

    Robert L. Stallings Milton Lamb | AIAA | 1982


    Wing-alone aerodynamic characteristics at high angles of attack

    Stallings, R. L., Jr. / Lamb, M. | NTRS | 1981


    Wing-alone aerodynamic characteristics at high angles of attack

    STALLINGS, JR., R. / LAMB, M. | AIAA | 1981


    Aerodynamic Characteristics of a Delta Wing at High Angles of Attack

    Oyama, A. / Imai, G. / Ogawa, A. et al. | British Library Conference Proceedings | 2008


    Aerodynamic Characteristics of a Delta Wing at High Angles of Attack

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