Johnson F T, Tinoco E N, Jong Y. Thirty years of development and application of CFD at Boeing commercial airplane, Seattle,AIAA-2003-3439[R]. Reston:AIAA,2003.
[2]
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.
[3]
Xu J, Liu Q H, Cai J S, et al. Drag prediction based on overset grids with implict hole cutting technique[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 208-217 (in Chinese). 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.
[4]
Zhang W S, Chen H X, Zhang Y F, et al. Nacelle strake'saerodynamic characteristics effects on high-lift configuration of transport aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(1): 76-85 (in Chinese). 张文升, 陈海昕, 张宇飞, 等. 短舱扰流片对运输机增升装置气动特性的影响[J]. 航空学报, 2013, 34(1): 76-85.
[5]
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.
[6]
Salas M D. Digital flight: The last CFD aeronaoutical grand challenge[J]. Journal of Scientific Computing, 2006,28(2-3): 479-505.
[7]
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: AIAA, 2002.
[8]
Laflin K R, Klausmeyer S M, Zickuhr T, et al. Data summary from the second AIAA computational fluid dynamics drag prediction workshop[J]. Journal of Aircraft, 2005, 42(5): 1165-1178.
[9]
Vassberg J C, Tinoco E N, Mani M, et al. Abridged summary of the third AIAA CFD drag prediction workshop[J]. Journal of Aircraft, 2008, 45(3): 781-798.
[10]
Vassberg J C, Tinoco E N, Mani M, et al. Summary of the fourth AIAA CFD drag prediction workshop, AIAA-2010-4547[R]. Reston: AIAA, 2010.
[11]
Levy D W, Laflin K R, Tinoco E N, et al. Summary of data from the fifth AIAA CFD drag prediction workshop, AIAA-2013-0046[R]. Reston: AIAA, 2013.
[12]
Hemsch M, Morrision J. Statistical analysis of CFD solutions for 2nd drag prediction workshop, AIAA-2005-0556[R]. Reston: AIAA, 2005.
[13]
Deng X G, Zhang H X. Developing high-order weightedcompact nonlinear schemes[J]. Journal of Computational Physics, 2000, 165(1): 24-44.
[14]
Deng X G, Mao M L, Tu G H, et al. Geometric conservation law and application to high-order finite difference scheme with stationary grid[J]. Journal of Computational Physics, 2011, 230(4): 1100-1115.
[15]
Deng X G, Min R B, Mao M L, et al. Further studies on geometric conservation law and application to high-order finite difference scheme with stationary grid[J]. Journal of Computational Physics, 2013, 239: 90-111.
[16]
Menter F R. Two-equation eddy-viscosity turbulence models for engineering application[J]. AIAA Journal, 1994, 32(8): 1598-1605.
[17]
Godard J L. F6 model tests in the ONERA S2MA wind tunnel[C]//The 2nd AIAA CFD Drag Prediction Workshop. Reston: AIAA, 2003.
[18]
Wang Y T, Wang G X, Zhang Y L. Validation of TRIP2.0: Numerical simulation of DPWII complex configuration[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(1): 34-40 (in Chinese). 王运涛, 王光学, 张玉伦. TRIP2.0软件的确认:DPWII复杂组合体的数值模拟[J]. 航空学报, 2008, 29(1): 34-40.
[19]
Vassberg J C, Tinoco E N, Mani M, et al. Comparison of NTF experimental data with CFD predictions from the third AIAA CFD drag prediction workshop, AIAA-2008-6918[R]. Reston: AIAA, 2008.
[20]
Tinoco E N. Drag prediction with the Zeus/CFL3D system, AIAA-2004-0552[R]. Reston: AIAA, 2004.