Wake integration method for airfoil drag evaluation using N-S equations

[1] Paterson J H, Blackerby W T, Schwanebeck J C. Analysis of flight test data on the C-141A aircraft . NASA CR-1558, Washington, D C:NASA, 1970 [2] MacWilkinson D G, Blackerby W T, Paterson J H. Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft——phase II, wind tunnel test, analysis, and prediction techniques . NASA CR-2333, Washington, D C:NASA,　1974 [3] Meredith P T. Viscous phenomena affecting high-lift systems and suggestions for future CFD development . High-Lift Systems Aerodynamics, AGARD CP 315 . London:Technical Editing and Reproduction, Ltd,1993 [4] 刘 周,朱自强,付鸿雁,等.高升阻比翼型的设计[J].空气动力学学报,2004,22(4):410~415 Liu Zhou, Zhu Ziqiang, Fu Hongyan, %et al%. Design of airfoil with high ratio of lift over drag[J]. Acta Aerodynamica Sinica,2004,22(4):410~415(in Chinese) [5] Tinoco E N. An assessment of CFD prediction of drag and other longitudinal characteristics . AIAA 2001-1002,2001 [6] Peavey C C. Drag prediction for military aircraft using CFD . AIAA 2000-0383,2000 [7] Van Dam C P. Recent experience with different methods of drag prediction[J]. Progress in Aerospace Sciences, 1999,35:751~798 [8] Van Dam C P, Nikfetrat K, Wong K. Drag prediction at subsonic and transonic speeds using Euler methods[J]. Journal of Aircraft, 1995,32(4):839~845 [9] 刘 杰,朱自强,陈泽民,等.基于欧拉方程的尾迹面法气动力计算[J].航空学报,2005,26(4):417~421 Liu Jie, Zhu Ziqiang, Chen Zemin, %et al%. Wake integration method for aerodynamics evaluation using Euler equations[J]. Acta Aeronautica et Astronautica Sinica,2005,26(4):417~421(in Chinese) [10] Chao D D, Van Dam C P. Airfoil drag prediction and decomposition . AIAA, 98-2783,1998 [11] Jameson A, Schmidt W, Turkel E. Numerical solutions of the Euler equations by finite volume methods with Runge-Kutta time stepping schemes . AIAA 81-1259,1981 [12] Baldwin B S, Lomax H. Thin layer approximation and algebraic model for separated turbulent flows . AIAA 78-257,1978 [13] Cook P H, McDonald M A, Firmin M C P. Aerofoil RAE2822-pressure distributions, and boundary layer and wake measurements . AGARD-AR-138, 1979