The invention discloses a long straight wing dynamics coupling wind tunnel test model with a resistance rudder, belongs to the technical field of tailless aircraft aeroelasticity wind tunnel models, and relates to a high aspect ratio wing dynamics coupling characteristic wind tunnel test model with a cracking type resistance rudder. The model comprises a basic model, a wing rigidity adjusting device, a control surface control rigidity adjusting device and a control surface deflection angle control device. Because the change of the rigidity distribution of the tailless aircraft wing can cause the change of the inherent frequency, the vibration characteristic of the tailless aircraft wing is influenced; change of control stiffness of the resistance rudder can be used for changing vibration characteristics of the control surface, and change of deflection angle of the control surface can be used for changing strength of attached vortexes. Therefore, the device provided by the invention canbe used for researching the dynamic coupling characteristic of the high aspect ratio wing with the cracking type resistance rudder.

    本发明公开了一种带有阻力舵的长直翼动力学耦合风洞试验模型,属于无尾飞机气动弹性风洞模型技术领域,是一种带有开裂式阻力舵的大展弦比机翼动力学耦合特性风洞试验模型,本发明包括基础模型、机翼刚度调整装置、舵面操纵刚度调节装置以及舵面偏角控制装置;由于无尾飞机机翼刚度分布的变化会导致其固有频率的变化,进而影响其振动特性;改变阻力舵操纵刚度可用于改变舵面的振动特性,改变舵面偏角可用于改变附着涡的强度。因此,采用本发明所述装置可研究带有开裂式阻力舵大展弦比机翼的动力学耦合特性。


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    Title :

    Long straight wing dynamic coupling wind tunnel test model with resistance rudder


    Additional title:

    一种带有阻力舵的长直翼动力学耦合风洞试验模型


    Contributors:
    ZHOU LI (author) / ZHOU DAHENG (author) / SHI YUAN (author) / QIU TAO (author)

    Publication date :

    2020-12-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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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