The invention provides a propeller-driven aircraft resistance characteristic calculation method considering dynamic influence. The influence of the attack angle, the speed, the engine tension, the engine number, the engine nacelle size and position, the tension line attack angle, the wing installation angle, the propeller diameter, the flap deflection angle, the flap chord length, the wing elongation and the aspect ratio, the propeller slip flow deflection angle and the slip flow viscosity loss on the resistance is fully considered, and the resistance coefficient of the propeller aircraft slip flow can be accurately obtained. The method is used for calculating the resistance generated by the slipstream of the propeller-driven aircraft, and can provide effective support for design, improvement and control of the propeller-driven aircraft.

    提供一种考虑动力影响的螺旋桨飞机阻力特性计算方法,充分考虑迎角、速度、发动机拉力、发动机数量、发动机短舱尺寸与位置、拉力线攻角、机翼安装角、螺旋桨直径、襟翼偏转角、襟翼弦长、机翼展长与展弦比、螺旋桨滑流偏角、滑流粘性损失对阻力的影响,可准确得出螺旋桨飞机滑流的阻力系数,用以螺旋桨飞机滑流产生阻力的计算,可为螺旋桨飞机的设计、改进及其操控提供有效支撑。


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    Title :

    Propeller aircraft resistance characteristic calculation method considering dynamic influence


    Additional title:

    一种考虑动力影响的螺旋桨飞机阻力特性计算方法


    Contributors:

    Publication date :

    2025-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / 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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