Simulation of aircraft in high lift configuration

Author:

Corjon A.1,Darracq D.1,Champagneux S.1,Gacherieu C.1,Svjoenfeld T.1

Affiliation:

1. CERFACS, Toulouse, France

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Potential hazard of aircraft wake vortices in ground effect with crosswind

2. lines at 12.03" 2Requier, C. S. and Duquesne, N. "Local preconditioning method applied for aerodynamic problems,"J. Aircraft, submitted 1999. 3Coa, H., Su, T., and Rogers, S. "Navier-Stokes analyses of a 747 high lift configuration," in 16th AIAA Applied Aerodynamics Conference, Albuquerque (AZ), No. AIAA-98-2623, June 19-22 1998. 4Mavriplis, D. and Pirzadeh, S. "Large-Scale parallel unstructured mesh computations for 3D high-lift analysis, " in 37'th AIAA Aerospace Sciences Meeting, Reno (NV), No. AIAA-99-0537, January 11-14 1999. 5Chow, J., Zilliac, G., and Bradshaw, P. "Mean and turbulent measurements in the near field of a wingtip vortex," AIAA Journal, Vol. 35, October 1997, pp. 1561-1567. 6Lockard, D. and Morris, P. "Wing-Tip Vortex Calculations Using a High-Accuracy Scheme," Journal of Aircraft, Vol. 35, No. 5, 1998, pp. 728-738. 7Khorrami, M., Singer, B., and R.H.Radeztsky, "Reynolds-Averaged Navier-Stokes Computations of a Flap-Side-Edge Flowfield," AIAA Journal, Vol. 37, January 1999, pp. 14-22. *Jameson, A., Schmidt, W., and Turkel, E. "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time Stepping," No. AIAA-81-1259, 1981. gDucros, F., Souleres, T., Laporte, F., Moinat, P., Weber, C., and Caruelle, B. "High-order skew

3. AIAA-99-3179

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Commercial aircraft wake vortices;Progress in Aerospace Sciences;2002-04

2. Prediction of high lift: review of present CFD capability;Progress in Aerospace Sciences;2002-02

3. Benchmark test for Euler calculations of a high lift configuration vortex wake;40th AIAA Aerospace Sciences Meeting & Exhibit;2002-01-14

4. Wake roll-up simulation up to the far-field;17th Applied Aerodynamics Conference;1999-06-28

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