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Effect of Finite Element Mesh and Load Location on the Stress and Deflection of a Light Aircraft Metal Wing Structure

机译：有限元网和负荷位置对轻型飞机金属翼结构应力和挠度的影响

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Mostefa BOURCHAK; Yousef DOBAH;
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1. Effect of Finite Element Mesh and Load Location on the Stress and Deflection of a Light Aircraft Metal Wing Structure [J] . Mostefa Bourchak, Yousef Dobah Transactions of the Japan society for aeronautical and space sciences . 2013,第2期

机译：有限元网格和载荷位置对轻型飞机金属机翼结构应力和挠度的影响
2. Bending Stress and Deflection Analysis of Meshing Spur Gear Tooth during the Single Tooth Contact with Finite Element Method and Determination of the Bending Stiffness [J] . Tsolakis Antonios D., Raptis Konstantinos G., Margaritou Maria D. American journal of engineering and applied sciences . 2017,第2期

机译：单齿接触时正齿轮啮合齿的弯曲应力与挠度的有限元分析及弯曲刚度的确定
3. Bending Stress and Deflection Analysis of Meshing Spur Gear Tooth during the Single Tooth Contact with Finite Element Method and Determination of the Bending Stiffness [J] . Antonios D. Tsolakis, Konstantinos G. Raptis, Maria D. Margaritou American journal of engineering and applied sciences . 2017,第2pta2期

机译：单齿接触时正齿轮啮合齿的弯曲应力和挠度的有限元分析及弯曲刚度的确定
4. Sensor Fusion Of Structural Finite Element Model With Inertial Sensor Data To Measure Wing Deflection Of A Fixed Wing Aircraft [C] . Georg Schirmer, James E. Steck AIAA SciTech Forum and Exposition . 2020

机译：带有惯性传感器数据的结构有限元模型的传感器融合，以测量固定翼飞机的机翼挠度
5. The development and use of a novel finite element for the evaluation of embedded fluid dampers within light-frame timber structures with seismic loading. [D] . Du, Ying. 2003

机译：新型有限元的开发和应用，用于评估轻型木结构在地震荷载作用下的嵌入式流体阻尼器。
6. 3-D finite element analysis of the effects of post location and loading location on stress distribution in root canals of the mandibular 1st molar [O] . Hong Gi YOON, Hyun Keun OH, Dong-Yul LEE, 2018

机译：下颌第一磨牙根管内桩位置和加载位置对应力分布影响的3-D有限元分析
7. Finite Element Analysis of Inter Spar Ribs of Composite Wing of Light Transport Aircraft against Brazier Load [O] . Polagangu James, Murali Krishna D, Gaddikeri KM, 2009

机译：轻型飞机复合机翼翼梁肋间抵抗火盆载荷的有限元分析
8. Large Deflection Analysis of Thin Elastic Structures by the Assumed Stress Hybrid Finite Element Method. [R] . boland,peter l. 1975

机译：基于假设应力混合有限元法的薄弹性结构大挠度分析。

Effect of Finite Element Mesh and Load Location on the Stress and Deflection of a Light Aircraft Metal Wing Structure

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