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EXTENSION OF THE NON-LINEAR HARMONIC METHOD TO FLOW COMPUTATIONS AROUND MOVING AND DEFORMING STRUCTURES

机译:非线性谐波方法在流动和变形结构周围流动计算的扩展

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Extensions to the existing Non-Linear Harmonic (NLH) method in presence of moving bodies are presented. The deformations of the structures are imposed through their natural mode shapes and complex generalized displacements. A harmonic mesh deformation is performed with a Radial Basis Function (RBF) interpolation. The harmonic flow equations are modified to incorporate the harmonic evolution of the mesh cells. The method is applied to pitching airfoils. Comparisons with full unsteady time-marching computations show a good agreement between bom approaches for subsonic flows. For transonic flows, to accurately follow the high non-linear effects due to the motion of shock position, the first order linearization of the harmonic equations has to be relaxed by taking into account the crossing terms into the harmonic equations. The NLH method has also been applied to turbomachinery aero-elastic effects, such as the STCF 11 axial turbine cascade. The results are in accordance with the experimental measurements.
机译:提出了在存在运动物体的情况下对现有非线性谐波(NLH)方法的扩展。结构的变形是通过其自然模式形状和复杂的广义位移来施加的。通过径向基函数(RBF)插值执行谐波网格变形。修改了谐波流方程,以合并网格单元的谐波演化。该方法适用于俯仰机翼。与完全非定常时间步长计算的比较表明,亚音速流的Bom方法之间具有良好的一致性。对于跨音速流,要准确地遵循由于激振位置的运动而产生的高非线性效应,必须通过考虑谐波方程中的交叉项来放宽谐波方程的一阶线性化。 NLH方法也已应用于涡轮机械的空气弹性效应,例如STCF 11轴向涡轮机叶栅。结果与实验测量结果一致。

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