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机译:非线性气动降阶模型的极限环颤振分析的有效方法
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, College of Aeronautics Northwestern Poly technical University, Xi'an 710072, China;
School of Aerospace Tsinghua University, Beijing 100084, China;
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, College of Aeronautics Northwestern Polytechnical University, Xi'an 710072, China;
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, College of Aeronautics Northwestern Polytechnical University, Xi'an 710072, China;
a: location of airfoil elastic axis; b: half-chord length; C_l: coefficients of lift; C_m: coefficients of pitch moment; c: number of neurons in the hidden layer; et al;
机译:极限循环振荡和颤振的非线性气动降阶模型
机译:一种新的长期内记忆神经网络的自我激发力模型,用于各种空气动力学配置的非线性颤动的极限周期振荡
机译:使用非定常空气动力学降阶模型对螺旋桨旋翼进行颤振分析
机译:基于非线性气动降阶模型降阶模型的极限环颤振分析的高效数值方法
机译:电力系统模型中极限循环的非线性分析。
机译:AEROM:NASA的非稳态气动和气动弹性降序建模软件
机译:非线性降阶建模用于极限循环振荡分析
机译:飞机机翼和机翼极限环振动的非线性降阶建模