机译:形状优化通过空气动力学不稳定伴随方法提高跨音质流体结构相互作用稳定性
Natl Key Lab Sci & Technol Aerodynam Design & Res Xian 710072 Peoples R China|Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China;
Natl Key Lab Sci & Technol Aerodynam Design & Res Xian 710072 Peoples R China|Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China;
Natl Key Lab Sci & Technol Aerodynam Design & Res Xian 710072 Peoples R China|Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China;
Natl Key Lab Sci & Technol Aerodynam Design & Res Xian 710072 Peoples R China|Northwestern Polytech Univ Sch Aeronaut Xian 710072 Peoples R China;
Unsteady adjoint method; Fluid-structure interaction; Single degree-of-freedom flutter; Stability; Shape optimization;
机译:伴随响应面法优化跨音速风扇的空气动力学形状
机译:基于伴随的流体结构交互存在形状优化问题的伴随方法
机译:单级跨音速压缩机的基于约束的伴随空气动力学形状优化
机译:跨声涡轮级的基于辅助的非定常气动优化
机译:Krylov-subspace方法具有动态放气,用于求解空气动力学优化方程的伴随方程
机译:对流轴流风机非定常空气动力相互作用的数值模拟
机译:一种新型非稳态空气动力学减少阶段空气弹性优化的空气动力学依次级模型方法
机译:X-37结构的气动外形优化提高了稳定性和性能