Emmons H W. The laminar-turbulent transition in a boundary layer-partⅠ[J]. Journal of Aerospace Science, 1951,18(7):490-498.
[2]
Abu-gharmam B J, Shaw R. Natural transition of boundary layers: the effects of turbulence, pressure gradient, and flow history[J]. Journal of Mechanical Engineering Science, 1980,22(5):213-228.
[3]
Bohn D, Heuer T. Conjugate flow and heat transfer calculations of a high-pressure turbine nozzle guide vane, AIAA-2001-3304[C/CD]//Proceedings of 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Salt Lake City: AIAA, 2001.
[4]
Facchini B, Magi A, Scotti A, et al. Conjugate heat transfer simulation of a radial cooled gas turbine vane, GT2004-54213[P/CD//Vienna: ASME, 2004.
[5]
Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated flows, AIAA-1978-257[C/CD]//Proceedings of AIAA 16th Aerospace Sciences Meeting. Huntsville: AIAA, 1978
[6]
Hylton L D, Milhec M S, Turner E R, et al. Analytical and experimental evaluation of the heat transfer distribution over the surface of turbine vanes, NASA-CR-168015[R/CD]//Indianapolis: NASA, 1983.
[7]
王松涛.叶轮机三维黏性流场数值方法与弯叶栅内涡系结构的研究[D].哈尔滨:哈尔滨工业大学,1999. Wang Songtao. Numerical method of 3D viscous flow field in turbomachinery and study of vortex structure in bowed blade cascade[D]. Harbin: Harbin Institute of Technology, 1999. (in Chinese)
[8]
Han Z X, Dennis B H. Simultaneous prediction of external flow-field and temperature in internally cooled 3-d turbine blade material, GT2000-253[P/CD]//New York: ASME, 2000.
[9]
Pulliam T H, Chaussee D S. A diagonal form of an implicit approximate factorization algorithm[J]. Journal of Computational Physics, 1981,39(2):371-390.
[10]
李荣华,冯果忱.微分方程数值解法[M].北京:高等教育出版社,1995. Li Ronghua, Feng Guochen. Dufferebtuak equation numerical resolution[M]. Beijing: Higher Education Press, 1995. (in Chinese)