, X.D.,Li, J.H.,Gao.Numerical Simulation of the Noise from Tandem Cylinder Flow with Spectral Difference Method.[会议录]:54th AIAA Aerospace Sciences Meeting
, D.K.,冯林, X.D., Li, J.H.,Gao.Numerical Simulation of the Noise from the 30P30N Highlift Airfoil with Spectral Difference Method.[会议录]:23rd AIAA/CEAS Aeroacoustics Conference
, X.D.,Li, X., Xu, J.H.,Gao.Numerical Simulation of Supersonic Twin-Jet Noise with High Order Finite Difference Scheme.[期刊]:AIAA Journal,2017
, X.D.,Li, J.H.,Gao.Implementation of Delayed Detached Eddy Simulation Method to a High Order Spectral Difference Solver.[期刊]:Computers and Fluids,2017,154:90-101
, X.D.,Li, J.H.,Gao.Improved Grid Block Interface Flux Reconstruction Method for High-Order Finite Difference Scheme.[期刊]:AIAA Journal,2015,53(7):1761-1773
, X.D.,Li, J.H.,Gao.Large Eddy Simulation of Supersonic Jet Noise from a Circular Nozzle:International Journal of Aeroacoustics,2011,10(4):465--474
, X.D.,Li, Z.G., Yang, J.H.,Gao.An Optimized Spectral Difference Scheme for CAA Problems:Journal of Computational Physics,2012,231:4848-4866
, J.H.,Gao.A block interface flux reconstruction method for numerical simulation with high order finite difference scheme:Journal of Computational Physics,2013,241:1-17
, J.H.,Gao, Q.,Wang.The drag-adjoint field of a circular cylinder wake at Reynolds numbers 20, 100 and 500:Journal of Fluid Mechanics,2015,730:145-161
, X.D.,Li, J.H.,Gao.Improved Grid Block Interface Flux Reconstruction Method for High-Order Finite Difference Scheme:AIAA Journal,2015,53(7):1761-1773
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