
的个人主页 http://faculty.ustc.edu.cn/gaoankang/zh_CN/index.htm
气动力诊断理论及其应用的研究进展
1,提出了基于压强泊松方程源项2 rho Q的加权积分的气动力分解方法
Gao, A.-K., Zou, S.-F., Shi, Y.-P. & Wu, J.-Z. 2019 Passing-over leading-edge vortex: the thrust booster in heaving airfoil. AIP Adv. 9 (3), 035314.10.1063/1.5064696
2,提出了气动力诊断中的局部伽利略不变性物理约束
Gao, A.-K. & Wu, J.-Z. 2019 A note on the Galilean invariance of aerodynamic force theories in unsteady incompressible flows. Acta Mech. Sinica 35, 1150–1154.
3,将气动力诊断理论应用到非均匀来流中
Luo, X.-G., Gao, A.-K. and Lu, X.-Y., 2023. Enhanced performance of a self-propelled flexible plate by a uniform shear flow and mechanism insight. Physics of Fluids, 35(2).
4,将气动力诊断理论应用到了三维流动问题中
Gao, A.-K., Cantwell, C.D., Son, O. and Sherwin, S.J., 2023. Three-dimensional transition and force characteristics of low-Reynolds-number flows past a plunging airfoil. Journal of Fluid Mechanics, 973, p.A43.
5,提出了基于加权积分的局部气动力诊断理论
Gao, A.-K., Xie, C.-Y. & Lu, X.-Y. 2025 Weighted integral methods for fluid force diagnostics in incompressible flows. J. Fluid Mech. 1024, A57.10.1017/jfm.2025.10854
目前,正在发展针对多相流、可压缩流动的气动力诊断理论。
气动力诊断软件
1,基于谱元法Nektar++的后处理工具
Performe force diagnostics in Nektar++ – Nektar++
2,基于二维lattice Boltzmann method和浸没边界方法的均匀网格数据的后处理工具