Investigation of engine jet/wing-tip vortex interference

Aerospace Science and Technology

Volumn 8, Issue 3, 2004, Pages 175-183

  Huppertz, Guido ^a   Fares, Ehab ^a   Abstiens, Ronald ^a   Schröder, Wolfgang ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

Engine; Jet; Numerical simulation; PIV; Vortex; Wake

Indexed keywords

AIRFOILS; COMPUTER SIMULATION; DIFFUSION; JET ENGINES; LIFT; MATHEMATICAL MODELS; VELOCITY MEASUREMENT; WAKES; WINGS;

FREE STREAM VELOCITY; GRIDS;

VORTEX FLOW;

EID: 1842530076     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2003.10.008     Document Type: Article

References (25)

1. Chow J.S., Zilliac G.G., Bradshaw P. Mean and turbulence measurements in the near field of a wingtip vortex. AIAA J. 35:(10):1997;1561-1567.
2. Dacles-Mariani J., Zilliac G.G., Chow J.S., Bradshaw P. Numerical/experimental study of a wingtip vortex in the near field. AIAA J. 33:(9):1995;1561-1568.
3. E. Fares, M. Meinke, W. Schröder, Numerical simulation of the interaction of wingtip vortices and engine jets in the near field, AIAA Paper, 2000-2222, 2000.
4. Fares E., Meinke M., Schröder W. Numerical simulation of the interaction of flap side-edge vortices and engine jets. ICAS 2000 Congress Proceedings. ICA0212 :2000.
5. Fares E., Schröder W. Zonal approach for the solution of the Navier-Stokes equations. ZAMM 2000. 80:(1):2000.
6. Fares E., Schröder W. Numerical simulation of wake flows. ECCOMAS CFD 2001 Congress Proceedings. 2001.
7. E. Fares, G. Huppertz, R. Abstiens, W. Schröder, Numerical and experimental investigation of the interaction of wing-tip vortices and engine jets in the near field, AIAA Paper, 2002-0403, 2002.
8. Garnier F., Brunet S., Jacquin L. Modelling exhaust plume mixing in the near field of an aircraft. Ann. Geophys. 15:1997;1468-1477.
9. T. Gerz, T. Ehret, Wake dynamics and exhaust distribution behind cruising aircraft, AGARD-CP-584, 35, 1996.
10. T. Gerz, F. Holzäpfel, D. Darracq, Aircraft wake vortices - a position paper, WakeNet Position Paper, 2001.
11. L. Jacquin, F. Garnier, On the dynamics of engine jets behind a transport aircraft, AGARD-CP-584, 35, 1996.
12. Jameson A. Solution of the Euler equations for two-dimensional transonic flow by a multigrid method. Appl. Math. Comp. 13:1983;327-355.
13. M.R. Khorrami, B.A. Singer, R.H. Radeztsky Jr., Reynolds averaged Navier-Stokes computations of a flap side-edge flow field, AIAA Paper, 98-0768, 1998.
14. + . J. Comput. Phys. 129:1996;164-382.
15. Liou M.S., Steffen Ch.J. A new flux splitting scheme. J. Comput. Phys. 107:1993;23-39.
16. Meinke M., Hänel D. Time accurate multigrid solutions of the Navier-Stokes equations. Hackbusch W., Trottenberg U. Multigrid Methods III. 1991;64-88 Birkhäuser.
17. Meinke M., Krause E. Simulation of incompressible and compressible flows on vector-parallel computers. Parallel Computational Fluid Dynamics: Proceedings of the Parallel CFD'98 Conference in Taiwan. 1999;25-34.
18. Paoli R., Laporte F., Cuenot B., Poinsot T. Dynamics and mixing in jet/vortex interactions. Phys. Fluids. 15:(7):2003;1843-1860.
19. Poinsot T.J., Lele S.K. Boundary conditions for direct simulations of compressible viscous flows. J. Comput. Phys. 101:1992;104-129.
20. Prasad A.K. Stereoscopic particle image velocimetry. Experiments in Fluids. vol. 29:2000;103-116 Springer-Verlag.
21. T.R. Quackenbush, M.E. Teske, A.J. Bilanin, Dynamics of exhaust plume entrainment in aircraft vortex wakes, AIAA Paper, 96-0747, 1996.
22. Raffel M., Willert Ch., Kompenhans J. Particle Image Velocimetry - A Practical Guide. 1998;Springer-Verlag, Berlin.
23. Spalart P.R. Airplane trailing vortices. Ann. Rev. Fluid Mech. 30:1998;107-138.
24. Thompson K.W. Time dependent boundary conditions for hyperbolic systems II. J. Comput. Phys. 89:1990;439-461.
25. van Leer B. Toward the ultimate conservative difference scheme V. A second-order. J. Comput. Phys. 32:1979;101-136.