[1] 阎超, 席柯, 袁武, 等. DPW系列会议评述与思考[J]. 力学进展, 2011, 41(6):776-784. YAN C, XI K, YUAN W, et al. Review of the drag prediction workshop series[J]. Advances in Mechanics, 2011, 41(6):776-784(in Chinese).[2] LEVY D W, ZICKUHR T, VASSBERG J C, et al. Summary of data from the first AIAA CFD drag prediction workshop:AIAA-2002-0841[R]. Reston,VA:AIAA, 2002.[3] LAFLIN K R, KLAUSMEYER S M, ZICKUHR T, et al. Summary of the second AIAA CFD drag prediction workshop[J]. Journal of Aircraft, 2005, 42(5):1165-1178.[4] VASSBERG J C, TINOCO E N, MANI M, et al. Summary of the third AIAA CFD drag prediction workshop[J]. Journal of Aircraft, 2008, 45(3):781-798.[5] VASSBERG J C, TINOCO E N, MANI M, et al. Summary of the fourth AIAA CFD drag prediction workshop:AIAA-2010-4547[R]. Reston,VA:AIAA, 2010.[6] SLOTNICK J, KHODADOUST A, ALONSO J, et al. CFD vision 2030 study:A path to revolutionary computational aerosciences:NASA/CR-2014-218178[R]. Washington, D. C.:NASA, 2014.[7] BARTH T J. An overview of combined uncertainty and a posteriori error bound estimates for CFD calculations:AIAA-2016-1062[R]. Reston,VA:AIAA, 2016.[8] 王运涛, 孟德虹, 孙岩, 等. DLR-F6/FX2B翼身组合体构型高精度数值模拟[J]. 航空学报, 2016, 37(2):484-490. WANG Y T, MENG D H, SUN Y, et al. High-order accuracy numerical simulation of DLR-F6/FX2B wing-body configuration[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(2):484-490(in Chinese).[9] JOHNSON F T, TINOCO E N, YU N J. Thirty years of development and application of CFD at Boeing Commercial Airplanes, Seattle[J]. Computer and Fluid, 2005, 34(10):1115-1151.[10] 张健, 邓有奇, 李彬, 等. 一种适用于三维混合网格的GMRES加速收敛新方法[J]. 航空学报, 2016, 37(11):3226-3235. ZHANG J, DENG Y Q, LI B, et al. A new method to accelerate GMRES's convergence applying to three-dimensional hybrid grid[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(11):3226-3235(in Chinese).[11] 徐嘉, 刘秋洪, 蔡晋生, 等. 基于隐式嵌套重叠网格技术的阻力预测[J]. 航空学报, 2013, 34(2):208-217. XU J, LIU Q H, CAI J S, et al. Drag prediction based on overset grids with implicit hole cutting technique[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2):208-217(in Chinese).[12] 王运涛, 李松, 孟德虹, 等. 梯形翼高升力构型的数值模拟技术[J]. 航空学报, 2014, 35(12):3213-3221. WANG Y T, LI S, MENG D H, et al. Numerical simulation technology of high lift trapezoidal wing configuration[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(12):3213-3221(in Chinese).[13] 康忠良, 阎超. 适用于混合网格的约束最小二乘重构方法[J]. 航空学报, 2012, 33(9):1598-1605. KANG Z L, YAN C. Constrained least-squares reconstruction method for mixed grids[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(9):1598-1605(in Chinese).[14] LEVY D W, CHAN M S. Comparison of viscous grid layer growth rate of unstructured grids on CFD drag prediction workshop results:AIAA-2010-4671[R]. Reston,VA:AIAA, 2010.[15] MAVRIPLIS D J. Viscous flow analysis using a parallel unstructured multigrid solver[J]. AIAA Journal, 2000, 38(11):2067-2076.[16] ALLMARAS S R, BUSSOLETTI J E. Algorithm issues and challenges associated with the development of robust CFD codes[R]. New York:Springer, 2009:1-19.[17] TINOCO E N, BOGUE D R, KAO T J, et al. Progress toward CFD for full flight envelope[J]. The Aeronautical Journal, 2005, 109(1100):451-460.[18] EMRE S, CHRISTOPH B. Gradient calculation methods on arbitrary polyhedral unstructured meshes for cell-centered CFD solvers:AIAA-2014-1440[R]. Reston,VA:AIAA, 2014.[19] SHIMA E, KITAMURA K, HAGA T. Green-Gauss/weighted-least-squares hybrid gradient reconstruction for arbitrary polyhedral unstructured grids[J]. AIAA Journal, 2013, 51(11):2740-2747.[20] ANDREW W C, ANDREW J D. Towards accurate flow predictions using unstructured meshes:AIAA-2009-3650[R]. Reston, VA:AIAA, 2009.[21] 张耀冰. 运输机气动特性混合网格数值模拟研究[D]. 绵阳:中国空气动力研究与发展中心, 2014. ZHANG Y B. Numerical simulation of transport aircraft's aerodynamic characteristics using mixed grid[D]. Mianyang:China Aerodynamics Research and Development Center, 2014(in Chinese).[22] BLAZEK J. Computational fluid dynamics:Principles and applications[M]. Oxford:Elsevier Science Ltd., 2001:129-179.[23] SAXENA S K, MANOJ T N. Implementation and testing of Spalart Allmaras model in a multi-block code:AIAA-2002-0835[R]. Reston,VA:AIAA, 2002.[24] REDEKER G. DLR-F4 wing body configuration, in Chapter B of a selection of experimental test cases for the validation of CFD codes:AGARD-1994-AR-303[R]. Paris:AGARD, 1994.[25] SHAHYAR Z P, NEAL T F. Assessment of the unstructured grid software TetrUSS for drag prediction of the DLR-F4 configuration:AIAA-2002-0839[R]. Reston,VA:AIAA, 2002.[26] TINOCO E, LEVY D. DWP 5 summary of participant da-ta[C]//5th CFD Drag Prediction Workshop. Reston, VA:AIAA, 2012.[27] 李钊, 陈海昕, 张宇飞. 基于广义Richardson外插方法的阻力预测精度分析[J]. 航空学报, 2015, 36(7):2105-2114. LI Z, CHEN H X, ZHANG Y F. Accuracy analysis of drag prediction based on generalized Richardson extrapolation[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(7):2105-2114(in Chinese).