ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2019, Vol. 40 ›› Issue (10): 23355-023355.doi: 10.7527/S1000-6893.2019.23355
• People Commemorate • Previous Articles Next Articles
WANG Baoguo1, HUANG Weiguang2, XU Yanji3
Received:
2019-08-08
Revised:
2019-08-13
Online:
2019-10-15
Published:
2019-08-20
CLC Number:
WANG Baoguo, HUANG Weiguang, XU Yanji. Professor Naixing Chen's main academic achievements and significant contributions to the development of science and technology: In memory of professor Naixing Chen's one-year anniversary[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(10): 23355-023355.
[1] | WU C H. A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types:NACA-TN-2604[R]. Washington, D.C.:NACA, 1952. |
[2] | 吴仲华. 使用非正交曲线坐标和非正交速度分量的叶轮机械三元流动基本方程及其解法[J]. 机械工程学报, 1979, 15(1):1-23. WU C H. Three-dimensional turbomachine flow equations expressed with respect to non-orthogonal curvilinear coordinates and non-orthogonal velocity components and methods of solution[J]. Journal of Mechanical Engineering, 1979, 15(1):1-23(in Chinese). |
[3] | WU C H. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines:NASA-CR-4496[R]. Washington, D.C.:NASA, 1993. |
[4] | 吴仲华论文选集编辑委员会. 吴仲华论文选集[M]. 北京:机械工业出版社, 2002. Editorial Committee on the Wu Chunghua Anthology. The Wu Chunghua anthology[M]. Beijing:China Machine Press, 2002(in Chinese). |
[5] | 陈乃兴.叶轮机械粘性气体气动热力学的若干问题——粘性项、传热项及基本方程的求解途径[J].中国科学(A辑),1983, 27(10):956-966. CHEN N X. Some problem in viscous gas flow in turbomachinery-Viscous and heat-transfer and methods for solution of basic equations[J]. Science in China, Ser. A, 1983, 27(10):956-966(in Chinese). |
[6] | 陈乃兴.任意非正交曲线坐标系在叶轮机械气动计算中的应用[J].工程热物理学报,1980, 1(2):110-119. CHEN N X. Application of non-orthogonal curvilinear coordinates to calculate the flow in turbomachines[J]. Journal of Engineering Thermophysics, 1980, 1(2):110-119(in Chinese). |
[7] | 陈乃兴.任意迴转S1流面叶栅可压附面层流动微分方程数值解[J].工程热物理学报,1987, 8(1):39-45. CHEN N X. Numerical solution of the boundary layer differential equations for cascades on the stream surface of revolution[J]. Journal of Engineering Thermophysics, 1987, 8(1):39-45(in Chinese). |
[8] | 陈乃兴,汪庆桓.S1流面叶栅附面层微分方程数值解(一)[J].工程热物理学报,1982, 3(2):151-157. CHEN N X, WANG Q H. Finite difference method for the boundary layer calculation of the cascade flow with S1 stream surface[J]. Journal of Engineering Thermophysics, 1982, 3(2):151-157(in Chinese). |
[9] | 汪庆桓,陈乃兴.非正交曲线坐标在叶轮机械粘性流动计算中的应用[J].工程热物理学报,1981, 2(4):320-327. WANG Q H, CHEN N X. Application of non-orthogonal curvilinear coordinates to calculate the viscous fluid flow in turbomahines[J]. Journal of Engineering Thermophysics, 1981, 2(4):320-327(in Chinese). |
[10] | 华耀南,陈乃兴.平面叶栅叶型的优化设计[J].工程热物理学报,1983, 4(3):248-254. HUA Y N, CHEN N X. Optimization of the plane compressor blade aerodynamic design[J]. Journal of Engineering Thermophysics, 1983, 4(3):248-254(in Chinese). |
[11] | 陈乃兴,张丰显.应用非正交曲线坐标表示的任意迴转流面叶栅粘性气体流动的完全N.S.方程的求解[J].中国科学(A辑),1984, 28(8):751-757. CHEN N X, ZHANG F X. A full Navier-Stokes solution of viscous gas flow through profile cascade on S1 stream surface of revolution employing non-orthogonal curvilinear coordinates[J]. Science in China, Series A, 1984, 28(8):751-757(in Chinese). |
[12] | 陈乃兴,李卫红.应用非正交曲线坐标系流函数方程求解任意迴转面叶栅的一种气动杂交问题[J].工程热物理学报,1986, 7(1):21-25. CHEN N X, LI W H. A new method for solving aerodynamic hybrid problem of profile cascade on S1 stream surface of revolution by employing stream function equation expressed with non-orthogonal coordinate system[J]. Journal of Engineering Thermophysics, 1986, 7(1):21-25(in Chinese). |
[13] | 陈乃兴,徐燕骥.透平叶栅中三维湍流的数值计算[J].科学通报, 1990, 35(14):69-72. CHEN N X, XU Y J. Numerical computation of 3-D turbulent flow in turbine cascade[J]. Chinese Sciences Bulletin, 1990, 35(14):69-72(in Chinese). |
[14] | CHEN N X, ZHANG F X. A generalized numerical method for solving direct, inverse and hybrid problems of blade cascade flow by using streamline coordinate equation:GT1987-29[R]. New York:ASME, 1987. |
[15] | CHEN N X, DAI L H. A time marching method for calculating S2 stream surface viscous flow in a single rotor compressor:GT1987-67[R]. New York:ASME, 1987. |
[16] | WANG B G, CHEN N X. An improved SIP scheme for numerical solutions of transonic streamfunction equations[J]. International Journal for Numerical Methods in Fluids, 1990(10):591-602. |
[17] | 王保国, 陈乃兴.一个高分辨率的矢通量分裂——TVD杂交新格式[J].应用力学学报, 1990, 7(2):83-89, 144. WANG B G, CHEN N X. A new high-resolution hybrid scheme of flux vector splittings-Hartens' TVD[J]. Chinese Journal of Applied Mechanics, 1990, 7(2):83-89,144(in Chinese). |
[18] | 王保国, 陈乃兴.计算流体中一个改进的强隐式格式及迭代的收敛性[J].计算物理,1989, 6(4):431-440. WANG B G, CHEN N X. An improved sip scheme and convergence analysis of the iterative procedure in fluid mechanics[J]. Chinese Journal of Computational Physics, 1989, 6(4):431-440(in Chinese). |
[19] | 陈乃兴, 董明,张家林.叶轮机械全三维气动杂交问题的数值求解方法[J].航空动力学报,1990, 5(2):97-102,185. CHEN N X, DONG M, ZHANG J L. Numerical solution of 3-D hybrid problem in turbomachinery[J]. Journal of Aerospace Power, 1990, 5(2):97-102,185(in Chinese). |
[20] | 黄伟光, 陈乃兴,山崎伸彦,等.叶轮机械动静叶片排非定常气动干涉的数值模拟[J].工程热物理学报,1999, 20(3):294-298. HUANG W G, CHEN N X, YAMASAKI N, et al. Numerical simulations on unsteady rotor-stator interaction in turbine cascades[J]. Journal of Engineering Thermophysics, 1999, 20(3):294-298(in Chinese). |
[21] | 陈乃兴, 黄伟光.无叶扩压器离心式压气机内旋涡运动的数值研究[J].工程热物理学报,1999, 20(2):155-160. CHEN N X, HUANG W G. Numerical study on vortices motions in the impeller of vaneless diffuser centrifugal compressor[J]. Journal of Engineering Thermophysics, 1999, 20(2):155-160(in Chinese). |
[22] | 陈乃兴, 徐燕骥,黄伟光,等.汽轮机小长径比静叶片的优化径向积叠[J].工程热物理学报,1998, 19(3):305-309. CHEN N X, XU Y J, HUANG W G, et al. On optimal radial-stacking of low span-diameter ratio steam turbine blades[J]. Journal of Engineering Thermophysics, 1998, 19(3):305-309(in Chinese). |
[23] | 黄伟光, 陈乃兴.透平叶栅气膜冷却效果的数值研究[J].工程热物理学报,1997, 18(6):677-682. HUANG W G, CHEN N X. Numerical computations of cooling effects by ejecting air from a slit on suction surface of a turbine blade[J]. Journal of Engineering Thermophysics, 1997, 18(6):677-682(in Chinese). |
[24] | 陈乃兴, 黄伟光,周倩.涡轮静叶周向和轴向弯曲对其气动性能影响的研究[J].工程热物理学报,1996, 17(3):286-290. CHEN N X, HUANG W G, ZHOU Q. A study on axial and circumferential skewing effect on some aerodynamic characteristics of a turbine stator[J]. Journal of Engineering Thermophysics,1996, 17(3):286-290(in Chinese). |
[25] | CHEN N X, ZHOU Q, HUANG W G. A study on axial skewing effect of a turbine stator by 3-D Navier-Stokes analysis:GT1996-149[R]. New York:ASME, 1996. |
[26] | 陈乃兴, 张丰显.透平级三维湍流流动的数值计算[J].工程热物理学报,1995, 16(2):156-160. CHEN N X, ZHANG F X. Numerical computation of 3-D turbulent flow in a turbine stage[J]. Journal of Engineering Thermophysics, 1995, 16(2):156-160(in Chinese). |
[27] | 聂超群, 陈静宜,陈乃兴,等.压缩系统喘振现象主动控制的实验研究[J].工程热物理学报,1995, 16(2):166-171. NIE C Q, CHEN J Y, CHEN N X, et al. Experimental study on active control surge in centrifugal compressor system[J]. Journal of Engineering Thermophysics, 1995, 16(2):166-171(in Chinese). |
[28] | 陈乃兴, 黄伟光,周倩.跨音速单转子压气机三维湍流流场的数值计算[J].航空动力学报,1995, 10(2):109-112. CHEN N X, HUANG W G, ZHOU Q. Numerical computation of 3D turbulent flow in a transonic single rotor compressor[J]. Journal of Aerospace Power, 1995, 10(2):109-112(in Chinese). |
[29] | 陈乃兴, 徐燕骥,黄伟光,等.单转子风扇的三维反问题气动设计[J].航空动力学报,2002, 17(1):23-28. CHEN N X, XU Y J, HUANG W G, et al. An inverse method for 3-D aerodynamic design of fans and pumps[J]. Journal of Aerospace Power, 2002, 17(1):23-28(in Chinese). |
[30] | 陈乃兴, 张宏武,徐燕骥,等.多级轴流压气机三维气动设计的一种快速方法[J].工程热物理学报,2003, 24(4):583-585. CHEN N X, ZHANG H W, XU Y J, et al. Numerical simulation of leakage flow in rotor tip clearance of a transonic turbine stage[J]. Journal of Engineering Thermophysics, 2003, 24(4):583-585(in Chinese). |
[31] | 张宏武, 陈乃兴,徐燕骥,等.跨音速单转子压气机气动设计的优化[J].工程热物理学报, 2005, 16(4):581-583. ZHANG H W, CHEN N X, XU Y J, et al. Optimal design of a transonic single rotor[J]. Journal of Engineering Thermophysics, 2005, 16(4):581-583(in Chinese). |
[32] | 王秀卓, 徐燕骥,陈乃兴.透平静叶的多参数气动优化设计方法[J].燃气轮机技术,2008, 21(2):22-27. WANG X Z, XU Y J, CHEN N X. Multi-parameter aerodynamic optimization method for a 3D turbine stator blades[J]. Gas Turbine Technology, 2008, 21(2):22-27(in Chinese). |
[33] | 陈乃兴, 张宏武,徐燕骥,等.叶型中弧线的最大弯度位置对跨音速压气机叶片性能影响的研究[J].工程热物理学报,2005, 26(3):409-412. CHEN N X, ZHANG H W, XU Y J, et al. Effect of maximum camber location on the aerodynamic performance of transonic compressor blades[J]. Journal of Engineering Thermophysics, 2005, 26(3):409-412(in Chinese). |
[34] | 张宏武, 徐燕骥,陈乃兴,等.跨音透平级动叶顶部间隙流动的数值模拟[J].工程热物理学报,2002, 23(4):441-444. ZHANG H W, XU Y J, CHEN N X, et al. Numerical simulation of leakage flow in rotor tip clearance of a transonic turbine stage[J]. Journal of Engineering Thermophysics, 2002, 23(4):441-444(in Chinese). |
[35] | WANG W S, LIANG X Z, CHEN N X. An experimental study on 3-D flow in an annular turbine cascade of high turning angle turbine blades[J]. Journal of Thermal Science, 1994, 3(2):89-92. |
[36] | CHEN N X. Aerothermodynamics of turbomachinery:Analysis and design[M]. Hoboken:John Wiley & Sons, 2010. |
[37] | 李根深, 陈乃兴, 强国芳. 船用燃气轮机轴流式叶轮机械气动热力学(原理、设计与试验研究):上册[M]. 北京:国防工业出版社, 1980. LI G S, CHEN N X, QIANG G F. Aerothermodynamics of axial turbomachinery for marin gas turbines:Vol. 1[M]. Beijing:Defense Industry Press, 1980(in Chinese). |
[38] | 李根深, 陈乃兴, 强国芳. 船用燃气轮机轴流式叶轮机械气动热力学(原理、设计与试验研究):下册[M]. 北京:国防工业出版社, 1985. LI G S, CHEN N X, QIANG G F. Aerothermodynamics of axial turbomachinery for marin gas turbines:Vol. 2[M]. Beijing:Defense Industry Press, 1985(in Chinese). |
[39] | 王保国. 《Aerothermodynamics of Turbomachinery》书评[J]. 航空学报, 2011, 32(2):377-378. WANG B G. Comments on Aerothermodynamics of Turbomachinery[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(2):377-378(in Chinese). |
[40] | FUJII K, DULIKRAVICH G S. Recent development of aerodynamic design methodologies:Inverse design and optimization[M]. Braunschweig:Vieweg & Sohn, 1999. |
[41] | 陈懋章. 航空发动机技术的发展[J]. 科学中国人, 2015(10):10-19. CHEN M Z. The tendency of aero-engine technology[J]. Scientific Chinese, 2015(10):10-19(in Chinese). |
[42] | 钱学森, 于景元, 戴汝为. 一个科学新领域——开放的复杂巨系统及其方法论[J]. 自然杂志, 1990, 13(1):3-10. TSIEN H S, YU J Y, DAI R W. A new discipline of science-The study of open complex giant system and its methodology[J]. Chinese Nature Magazine, 1990, 13(1):3-10(in Chinese). |
[43] | 王保国, 黄伟光, 徐燕骥, 等. 航空涡扇发动机多目标多学科设计优化方法[M]. 北京:机械工业出版社, 2019. WANG B G, HUANG W G, XU Y J, et al. Methods for multidisciplinary design optimization of aero-turbofan engine[M]. Beijing:China Machine Press, 2019(in Chinese). |
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