[1] Morino L, Kuo C C. Subsonic potential aerodynamics for complex configurations: A general theory[J]. AIAA Journal, 1974, 12(2): 191-197.
[2] Liu Q G. The uniqueness of the solution of the velocity potential integral equation established by using Green's theorem[J]. Journal of Northwestern Polytechnical University, 1978(1): 139-145 (in Chinese). 刘千刚.关于用格林定理建立的物面速势积分方程解的唯一性问题[J].西北工业大学学报, 1978(1): 139-145.
[3] Liu Q G. Review of the Green's function method for steady and unsteady, subsonic, transonic and supersonic aerodynamics around complex configuration[J]. Acta Aeronautica et Astronautica Sinica, 1996, 17(2): 137-143 (in Chinese). 刘千刚. 复杂构形的亚、跨、超音速定常及非定常气动力的Green函数算法综述[J]. 航空学报, 1996, 17(2): 137-143.
[4] Hess J L. Review of integral equation techniques for solving potential flow problems with emphasis on the surface-source method[J]. Computer Methods in Applied Mechanics and Engineering, 1975, 5: 145-196.
[5] Chmitt V S, Charpin F. Pressure distributions on the ONERA-M6-wing at transonic Mach numbers, AGARD AR-138[R]. [S.l.]: AGARD, 1979.
[6] Gao Z L, Zou Z J.A three-dimensional desingularized high order panel method based on NURBS[J].Journal of Hydrodynamics, 2008, 20(2): 137-146.
[7] Chen Z M.A vortex based panel method for potential flow simulation around a hydrofoil[J]. Journal of Fluid and Structures, 2012(28): 379-391.
[8] Richard L F. Airfoil aerodynamics using panel method[J]. The Mathematical Journal, 2008, 10(4): 725-739.
[9] Cheng B L, Cranfill C W, Axford R. Using the Green's function method to calculate pressure fluctuations in compressible multifluid[C]//Proceedings of the 9th International Workshop on the Physics of Compressible Turbulent Mixing. Cambridge: [s.n.], 2004: 1-14.
[10] Tan J F, Wang H W. Panel/full-span free wake coupled method for unsteady aerodynamic of a helicopter rotor blade[J]. Chinese Journal of Aeronautics, 2013, 26(3): 535-543.
[11] Markus D, Manuel K, Ewald K, et al. Tip vortex conservation on a helicopter main rotor using vortex-adapted chimera grids[J]. AIAA Journal, 2007, 45(8): 2062-2074.
[12] Liang H, Zong Z, Zou L, et al. Vortex shedding from a two-dimensional cylinder beneath a rigid wall and a free surface according to the discrete vortex method[J]. European Journal of Mechanics B/Fluids, 2014, 43: 110-119.
[13] Ji J C, Bai L, Huang X. A state observer based algorithm for aeroacoustic beamforming[J]. Acta Aeronautica et Astronautic Sinica, 2011, 25(1): 35-40 (in Chinese). 季建朝, 白龙, 黄迅. 基于状态观测器的波束行成算法及其航空应用[J]. 航空学报, 2011, 25(1): 35-40.
[14] Xu J H, Song W P, Han Z H. Prediction of aeroacoustic noise for helicopter rotors based on vorticity confinement method[J]. Acta Aeronautica et Astronautic Sinica, 2011, 25(12): 2204-2212 (in Chinese). 徐建华, 宋文萍, 韩忠华. 基于涡限制法的旋翼气动噪声计算[J]. 航空学报, 2011, 25(12): 2204-2212.
[15] Francescantonio P D, Casalino D. Green's function discretization scheme for sound propagation in nonuniform flows[J]. AIAA Journal, 1999, 37(10): 1161-1172. |