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机译:使用详细的实验数据验证和改进机翼后缘噪声预测模型
Institute of Aerodynamics and Gas Dynamics (IAG), Universitat Stuttgart, Pfaffenwaldring 21, D-70550 Stuttgart, Germany;
Institute of Aerodynamics and Gas Dynamics (IAG), Universitat Stuttgart, Pfaffenwaldring 21, D-70550 Stuttgart, Germany;
Institute of Aerodynamics and Gas Dynamics (IAG), Universitat Stuttgart, Pfaffenwaldring 21, D-70550 Stuttgart, Germany;
Department of Mechanical Engineering, Technical University of Denmark (DTU), Nils Koppels Alls, Building 403, DK-2800 Lyngby, Denmark;
Department of Mechanical Engineering, Technical University of Denmark (DTU), Nils Koppels Alls, Building 403, DK-2800 Lyngby, Denmark;
Department of Mechanical Engineering, Technical University of Denmark (DTU), Nils Koppels Alls, Building 403, DK-2800 Lyngby, Denmark;
Wind Energy Division, Rise-DTU, Building 118, DK-4000 Roskilde, Denmark;
Wind Energy Division, Rise-DTU, Building 118, DK-4000 Roskilde, Denmark;
turbulent boundary-layer; trailing-edge noise; wall pressure fluctuation; far-field noise spectrum; two-point correlation;
机译:基于经验壁压谱模型的机翼后缘噪声预测
机译:翼型后缘噪声预测的半经验表面压力谱模型
机译:旋转叶片尾缘噪声:分析模型的实验验证
机译:“QBLADE”内部“PNOISE”翼型后辐射边缘噪声预测模块的验证和验证
机译:分数齐纳本构模型描述猪脑的退化,并通过实验数据和有限元分析的预测进行验证
机译:TAS2R38苦味受体的粗粒/分子力学:激动剂结合的实验验证的详细结构预测
机译:旋转叶片后缘噪声:分析模型的实验验证