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Modeling of the FWD Deflection Basin to Evaluate Airport Pavements

机译:FWD转向盆建模以评估机场路面

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The falling weight deflectometer (FWD) testing develops a deflection basin on the pavement surface. Depths of this deflection basin from the center of the falling weight are measured at different radial offsets. These deflections are used for the backcalculation of the pavement layer moduli. Most of the available backcalculation software uses the layered elastic theory and static load to calculate moduli from known pavement surface deflections. However, the FWD test load is dynamic, and layer materials may show nonelastic behavior. Layered elastic theory in these types of software cannot characterize dynamic response of the pavement. Also, elastic theory is unable to accurately predict the surface deflection whenever stress developed in any pavement layer exceeds the yield point. For this reason, this study has performed a finite-element analysis of the airport pavement under the FWD test considering the dynamic load and materials plasticity. The analysis presented here includes elastoplastic behavior of pavement layer materials. Both axisymmetric and quarter cube models have been developed in ABAQUS. Time-deflection histories are simulated to match the FWD test data. A comparison is made between the dynamic, static, and field deflection basins. Contours of vertical deflection and strain are also plotted to observe their distribution on both the axisymmetric and quarter cube models. Analysis results show that the time-deflection histories are in close agreement with the field data. The axisymmetric model yields better results than the quarter cube model. Deflections from the static analysis are greater than the dynamic analysis for an identical set of the layer modulus of ; elasticity. A uniform distribution of strain is observed from the static analysis in both of the geometries. However, the dynamic analysis does not show similar distribution because of the time-dependent response.
机译:落锤挠度计(FWD)测试在人行道表面形成了一个偏斜盘。在不同的径向偏移处测量该偏转盆距落锤中心的深度。这些挠度用于路面层模量的反算。大部分可用的反算软件都使用分层弹性理论和静载荷从已知路面的表面挠度计算模量。但是,FWD测试载荷是动态的,并且层材料可能显示出非弹性行为。这些类型的软件中的分层弹性理论无法描述路面的动态响应。而且,只要在任何路面层中产生的应力超过屈服点,弹性理论都无法准确预测表面变形。因此,本研究在FWD试验下对机场路面进行了有限元分析,考虑了动态载荷和材料可塑性。这里介绍的分析包括路面层材料的弹塑性行为。轴对称模型和四分之一立方模型均已在ABAQUS中开发。模拟时变历史以匹配FWD测试数据。在动态,静态和场偏转盆之间进行了比较。还绘制了垂直挠度和应变的轮廓,以观察它们在轴对称和四分之一立方模型上的分布。分析结果表明,时变历史与现场数据非常吻合。轴对称模型比四分之一立方模型产生更好的结果。对于相同的层模量集,静态分析的偏差大于动态分析的偏差;弹性。通过静态分析,在两种几何结构中均观察到应变的均匀分布。但是,由于时间相关的响应,动态分析未显示相似的分布。

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