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Advanced aeroelastic simulations for practical fixed-wing and rotary-wing applications.

机译:适用于固定翼和旋翼应用的高级气动弹性仿真。

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The study of aeroelasticity has many applications in the aerospace industry. There is a need in the fixed-wing and rotary-wing fields to develop computational aeroelastic tools for industrial applications that are both rapid and robust. Aeroelastic tools that would benefit the industry were developed in this work to predict the transonic fixed-wing flutter boundary and to predict rotary-wing wind turbine performance.;The flutter boundary of a wing must be determined during development and certification of an aircraft, and is critical in the transonic regime, where nonlinear effects create a dip in the flutter boundary that cannot be predicted with traditional linear tools. A frequency domain correction procedure was developed to account for nonlinear aerodynamics in the transonic regime. The flutter boundary of the experimental benchmark AGARD 445.6 wing was calculated using time domain and corrected frequency domain methods. Both approaches adequately predicted the flutter boundary, but the corrected frequency domain approach is significantly faster than the time domain simulations and represents a unique opportunity for improved flutter prediction during aircraft wing design and development.;Wind turbines represent a rapidly growing source of renewable energy but current predictive tools have been shown to lack accuracy in predicting the power output of wind turbines. Additionally, wind farm performance must be properly predicted to develop accurate annual energy estimates. An aeroelastic, aeroacoustic, discrete vortex method code called SMARTROTOR was used to predict the performance of the benchmark National Renewable Energy Laboratory (NREL) wind turbine experiment. The code properly predicted the NREL wind turbine performance in normal and yawed flow conditions and has demonstrated the capability of simulating the wake interference effects present in wind farms. The grid-free characterization of the wake behind the turbine and the rapid simulation time compared with grid-based computational fluid dynamics solvers highlights the relevance of the code for industrial applications.
机译:空气弹性的研究在航空航天工业中有许多应用。在固定翼和旋转翼领域中需要开发既快速又坚固的用于工业应用的计算气动弹性工具。在这项工作中开发了对行业有利的气动弹性工具,以预测跨音速固定翼扑翼边界并预测旋翼风力涡轮机性能。;必须在飞机的开发和认证过程中确定机翼的扑翼边界;以及在跨音速模式中至关重要,非线性影响会在颤振边界中产生一个使用传统线性工具无法预测的下降。开发了频域校正程序来解决跨音速状态下的非线性空气动力学问题。实验基准AGARD 445.6机翼的扑动边界是使用时域和校正频域方法计算的。两种方法都可以充分预测颤振边界,但是校正后的频域方法比时域仿真要快得多,并且为飞机机翼设计和开发过程中改进颤振预测提供了独特的机会。风轮机代表了可再生能源的快速增长,但已经显示出当前的预测工具在预测风力涡轮机的功率输出方面缺乏准确性。此外,必须正确预测风电场的性能,以开发准确的年度能源估算。使用称为SMARTROTOR的气动弹性,气动声学,离散涡旋方法代码来预测基准国家可再生能源实验室(NREL)风力涡轮机实验的性能。该代码正确地预测了NREL风力涡轮机在正常和偏航条件下的性能,并展示了模拟风电场中尾流干扰影响的能力。与基于网格的计算流体动力学求解器相比,涡轮机尾流的无网格特征和快速的仿真时间突显了该代码与工业应用的相关性。

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