武鹏.喷管间距对双喷流啸音影响的实验:航空动力学报,2018,33(1)
张东飞.GPU加速高阶谱差分方法在风扇噪声中的应用研究.[期刊].北京:航空学报,2024,45(8):128941
Gao, J.H.,Li, X.D..Numerical Simulation of the Noise from Tandem Cylinder Flow with Spectral Difference Method.[会议录]:54th AIAA Aerospace Sciences Meeting
,Gao, J.H.,X.D., Li,D.K., Lin.Numerical Simulation of the Noise from the 30P30N Highlift Airfoil with Spectral Difference Method.[会议录]:23rd AIAA/CEAS Aeroacoustics Conference
Gao, J.H.,Li, X.D.,Xu, X..Numerical Simulation of Supersonic Twin-Jet Noise with High Order Finite Difference Scheme.[期刊]:AIAA Journal,2017
Gao, J.H.,Li, X.D..Implementation of Delayed Detached Eddy Simulation Method to a High Order Spectral Difference Solver.[期刊]:Computers and Fluids,2017,154:90-101
Gao, J.H.,Li, X.D..Improved Grid Block Interface Flux Reconstruction Method for High-Order Finite Difference Scheme.[期刊]:AIAA Journal,2015,53(7):1761-1773
Gao, J.H.,Li, X.D..Large Eddy Simulation of Supersonic Jet Noise from a Circular Nozzle:International Journal of Aeroacoustics,2011,10(4):465--474
Gao, J.H.,Li, X.D.,Yang, Z.G..An Optimized Spectral Difference Scheme for CAA Problems:Journal of Computational Physics,2012,231:4848-4866
Gao, J.H..A block interface flux reconstruction method for numerical simulation with high order finite difference scheme:Journal of Computational Physics,2013,241:1-17