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TRIGONOMETRIC INTERPOLATION METHOD FOR EFFICIENT DETERMINATION OF TURBOMACHINERY BLADE FLUTTER CHARA
[会议论文] 作者：Xiuquan Huang,Ding Xi Wang,
来源：第三届中国国际透平机械学术会议 年份：2018
Proposed in the paper is a trigonometric interpolation method for efficient determination of turbomachinery blade flutter characteristic curves.The trigonometric interpolation is incorporated with the...
[会议论文] 作者：Hengming Zhang,Xiuquan Huang,Xiang Zhang,
来源：7th International Conference on Fluid Mechamics(ICFM7)(第七届国际 年份：2015
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[会议论文] 作者：Xiang Zhang,Xiuquan Huang,Hengming Zhang,Xuefeng Li,
来源：7th International Conference on Fluid Mechamics(ICFM7)(第七届国际 年份：2015
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[会议论文] 作者：TAN Lijun,FANG Bo,QU Xiuquan,HUANG Wenhu,
来源：第十四届全国非线性振动会议暨第十一届全国非线性动力学和运动稳定性学术会议 年份：2013
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[会议论文] 作者：Zhihao Wu,Dingxi Wang,Xiuquan Huang,Shenren Xu,
来源：第三届中国国际透平机械学术会议 年份：2018
Most established flow simulation tools,although constantly being perfected to compute the flow accurately,are inherently incapable of predicting the regime the flow being simulated is operating in.One...
Nonlinear uncertainty quantification of the impact of geometric variability on compressor performanc
[期刊论文] 作者：Qian ZHANG,Shenren XU,Xianjun YU,Jiaxin LIU,Dingxi WANG,Xiuquan HUANG,
来源：中国航空学报（英文版） 年份：2022
Manufactured blades are inevitably different from their design intent,which leads to a deviation of the performance from the intended value.To quantify the associated performance uncertainty,many approaches have been developed.The tradition......
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