Citation: | Zhou Yu, Yan Chao. Entropy correction analyses for Roe scheme[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(3): 356-360. (in Chinese) |
[1] Roe P L. Approximate Riemann solvers parameter vectors and difference schemes[J]. Journal of Computational Physics, 1981,43(2):357-372 [2] 阎超. 计算流体力学方法及应用[M].北京: 北京航空航天大学出版社, 2006: 64-66 Yan Chao. Computational fluid dynamics method and application[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2006:64-66 (in Chinese) [3] Muller B. Simple improvements if an upwind TVD scheme for hypersonic flow . AIAA-89-1977, 1989 [4] Yee H C. Upwind and symmetric shock-capturing schemes . NASA-TM-89464, 1987 [5] Harten A , Hyman J M. Self-adjusting grid methods for one-dimensional hyperbolic conservation laws [J]. Journal of Computational Physics, 1983, 50(2):235-269 [6] Kermani M J, Pleet E G. Modified entropy correction formula for the roe scheme . AIAA-2001-0083, 2001 [7] Sanders R, Morano E, Druguet M C. Multidimensional dissipation for upwind schemes: stability and applications to gas dynamics [J]. Journal of Computational Physics, 1998, 145(2):511-537 [8] Woodward P, Colella P. The numerical simulation of two dimensional fluid flow with strong shocks [J]. Journal of Computational Physics, 1984, 54(1): 115-173 [9] Anderson D J. Computational fluid dynamics: the basis with applications [M]. New York: McGraw-Hill, 1995:502-504 [10] Maurizio P, Domenic D. Numerical instabilities in upwind methods: analysis and cures for the "carbuncle" phenomenon[J]. Journal of Computational Physics, 2001, 166(2):271-301 [11] 谢锦睿,吴颂平.TVD格式与高超音速气动加热数值模拟[J].北京航空航天大学学报, 2007, 33(4):392-396 Xie Jinrui,Wu Songping. TVD scheme and numerical simulation of aerodynamic heating in hypersonic flows[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(4):392-396 (in Chinese)
|
[1] | LU X,SUN Y N,TANG J,et al. Kinematic characteristics analysis of vehicle-aircraft towing taxi system considering wheel deformation[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(2):478-486 (in Chinese). doi: 10.13700/j.bh.1001-5965.2023.0029. |
[2] | ZHANG K,YAO Y P. Optimization analysis for numerical calculation of UH model[J]. Journal of Beijing University of Aeronautics and Astronautics,2025,51(2):546-552 (in Chinese). doi: 10.13700/j.bh.1001-5965.2023.0001. |
[3] | SU Jinxin, XI Ziyan, DAI Yuting. Nonlinear fluid-structure interaction response analysis of a large flexible wing under strong gusts[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0278 |
[4] | YU Rui, WANG Xiaojun, HE Xiaoying, LI Biao. Simulation and analysis of ignition flow field in granular propellant gas generators[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0683 |
[5] | ZHANG Xin-ze, LI Qin, WENG Yi-hui, YOU Yan-cheng. Numerical analysis and flow state prediction of double wedge steady/unsteady flow at different Ma∞、Re[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0758 |
[6] | LIU Y X,LIU Z H,GAO Q H,et al. Joint estimation algorithm of vertical force and lateral force of heavy-duty tire based on internal strain analysis of tire[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(11):3532-3541 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0816. |
[7] | LI Yijian, ZHOU Jianghua, ZHANG Xiaojun, ZHAO Chunyang, XU Guoning. Dynamic modeling and control analysis of pitch/roll channels in the ball cabin system[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0356 |
[8] | LEI Juan-mian, ZHU Pei-yu. Numerical Study on Lateral Jet Control Efficiency of Hypersonic Reentry Double-cone Vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0714 |
[9] | ZOU L,WU W N,LIU J,et al. Numerical simulation of flow around two tandem wavy conical cylinders at subcritical Reynolds number[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(3):706-715 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0285. |
[10] | WU Z Y,GAO Z X,CHEN X M,et al. Mach number effect in shock-wave/turbulent-boundary-layer interaction flow[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(11):3484-3494 (in Chinese). doi: 10.13700/j.bh.1001-5965.2022.0857. |
[11] | LI Z B,SUN W,ZHANG Y N,et al. Computation on aerodynamic and aeroacoustic characteristics of scissor tail-rotor under sideslip condition[J]. Journal of Beijing University of Aeronautics and Astronautics,2024,50(12):3794-3805 (in Chinese). doi: 10.13700/j.bh.1001-5965.2023.0037. |
[12] | WANG Xiao, MA Jun, XIONG Xin, CHEN Jing-yu. Dynamic modeling and analysis of rolling bearing with raceway spalling defect[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0565 |
[13] | YANG Yi-feng, WANG Yi, LIU Ao-yu, LI Jia, XIE Li-yang. Calculation and error analysis of kinematic accuracy reliability of VSV adjustment mechanism[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0410 |
[14] | ZHAO T M,HOU J X,LIU Y W. Influence mechanism of continuous curvature shaping method on buzz-saw noise[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(4):922-931 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0342. |
[15] | GUO S N,SONG W,XIANG N L,et al. Dynamic characteristics of turbine flowmeter based on CFD simulation[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(8):1904-1911 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0594. |
[16] | GAO J C,CHEN W J,HU W J,et al. Analysis of CO2 distribution characteristics in cabin of civil aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics,2023,49(9):2510-2517 (in Chinese). doi: 10.13700/j.bh.1001-5965.2021.0683. |
[17] | LI Yongchang, DAI Yuting, YANG Chao. Fluid and structure coupling analysis of split drag rudder[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2494-2501. doi: 10.13700/j.bh.1001-5965.2021.0151 |
[18] | PENG Cheng, SUN Liguo, WANG Yanyang, TAN Wenqian, XIAO Feng. Control oriented longitudinal modeling and analysis of pigeon-like flapping-wing aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2510-2519. doi: 10.13700/j.bh.1001-5965.2021.0130 |
[19] | WENG Huiyan, CAI Guobiao, ZHENG Hongru, LIU Lihui, ZHANG Baiyi, HE Bijiao. Numerical simulation of effect of background pressure on electric propulsion plume field[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1854-1862. doi: 10.13700/j.bh.1001-5965.2021.0039 |
[20] | GONG Xiaoquan, WU Xiaojun, TANG Jing, LI Ming, ZHANG Jian. Application of r-grid adaptive for shock capturing in discontinuous Galerkin finite element method[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(10): 1889-1898. doi: 10.13700/j.bh.1001-5965.2021.0046 |