On the structure of the shear layer emanating from a swept leading edge at angle of attack

33rd AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Visbal, M R ^a   Gordnier, R E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894622644     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (46)

1. D Rockwell. Three-Dimensional Flow Structure on Delta Wings at High Angle of Attack: Experimental Concepts and Issues. AIAA Paper 93-0550, 1993.
2. M R. Visbal. Computational and Physical Aspects of Vortex Breakdown on DeltaWings. AIAA-95-0585, January 1995.
3. H.B. Squire, J.G. Jones, and A. Stanbrook. Investigation of the Characteristics of Some Plane and Cambered 65 Deg Delta Wings at Mach Numbers from 0,7 to 2.0. ARC, R.M. No. 3305, 1961.
4. M Gad-el-Hak and R. F. Blackwelder, The Discrete Vortices from a Delta Wing. AIAA Journal, 23(6):961-962, June 1985.
5. M Gad-el Hak and R. F. Blackwelder. Control of the Discrete Vortices from a Delta Wing. AIAA, 25(8):1042-1049, 1987.
6. F.M Payne, T. T. Ng, R. C. Nelson, and L. B. Schiff. Visualization and Wake Surveys of Vortical Flow over a Delta Wing. AIAA Journal, 26(2): 137-143, February 1988.
7. M V. Lowson. The Three Dimensional Vortex Sheet Structure on Delta Wings. In Fluid Dynamics of ThreeDimensional Turbulent Shear Flows and Transition, October 1987 AGARD-CP-438.
8. G. A. Reynolds and A. A. Abtahi. Three-Dimensional Vortex Development, Breakdown, and Control. AIAA-89-0998, March 1989.
9. M V. Lowson, A. J. Riley, and C. Swales. Flow Structure over Delta Wings. AIAA-95-0586, January 1995.
10. J. Riley and M.V. Lowson. Development of a ThreeDimensional Eree Shear Layer. JFM, 369:49-89, 1998.
11. N.G. Verhaagen, J.P Meeder, and J.M Verhelst. Boundary Layer Effects on the Flow of a Leading Edge Vortex. AIAA Paper 93-3463-CP, 1993.
12. E. Washburn and K. D. Visser. Evolution of Vortical Structures in the Shear Layer of Delta Wings. AIAA-94-2317, June 1994.
13. Mitchell, P. Molton, Barberis D, and J. Delery. Vortical Substructures in the Shear Layers Forming Leading-Edge Vortices. AIAA Paper 2001-2424, 2001.
14. R. E. Gordnier and M R. Visbal. Numerical Simulation of the Unsteady Vortex Structure over a Delta Wing. AIAA-91-1811, June 1991.
15. R. E. Gordnier and M R. Visbal. Unsteady Vortex Structure over a Delta Wing. Journal of Aircraft, 31(1):243-248, Jan.-Feb. 1994.
16. Mitchell, S. Morton, and J. Forsythe. Analysis of Delta Wing Vortical Substructures Using Detached-Eddy Simulation. AIAA Paper 2002-2968, 2002.
17. M R. Visbal and R. E. Gordnier. Ori gin of Computed Unsteadiness in the Shear Layer of Delta Wings. Journal of Aircraft, 32(5):1146-1148, 1995.
18. R.E. Gordnier and M.R. Visbal. Instabilities in the Shear layer of Delta Wings. AIAA Paper 1995-2281, 1995.
19. K. M. Cipolla and D. Rockwell. Small-Scale Vortical Structures in Crossflow Plane of a Rolling Delta Wing. AIAA, 36(12):2276-2278, 1998.
20. M R Visbal and D.V. Gaitonde, High-Order Accurate Methods for Complex Unsteady Subsonic Flows. AIAA Journal, 37(10):1231-1239, 1999.
21. M. Vinokur. Conservation Equations of Gasdynamics in Curvilinear Coordinate Systems. Journal of Computational Physics, 14:105-125, 1974.
22. J.L. Steger. Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional Geometries. AIAA Journal, 16(7):679-686, 1978.
23. D.A. Anderson, J.C. Tannehill, and R.H. Pletcher, Computational Fluid Mechanics and Heat Transfer, McGraw-Hill Book Company, 1984.
24. M.R. Visbal and D.V. Gaitonde. On the Use of High-Order Finite-Difference Schemes on Curvilinear and Deforming Meshes. Journal of Computational Physics, 181:155-185, 2002.
25. S.K. Lele. Compact Finite Difference Schemes with Spectral-like Resolution. Journal of Computational Physics, 103:16-42, 1992.
26. D V Gaitonde and M. R. Visbal. High-Order Schemes for Navier-Stokes Equations: Algorithm and Implementation into FDL3DI. Technical Report AFRL-VA-WP-TR-1998-3060, Air Force Research Laboratory, Wright-Patterson AFB, 1998.
27. DV. Gaitonde, J.S. Shang, and J.L. Young. Practical Aspects of Higher-Order Numerical Schemes for Wave Propagation Phenomena. Int. Jnl. for Num. Methods in Eng., 45:1849-1869, 1999.
28. P. Alpert. Implicit Filtering in Conjunction with Explicit Filtering. J. Comp. Phys., 44:212-219, 1981.
29. D V. Gaitonde and M.R. Visbal. Further Development of a Navier-Stokes Solution Procedure Based on Higher-Order Formulas. AIAA Paper 99-0557, January 1999.
30. M. Visbal and D. Gaitonde. Very High-Order Spatially Implicit Schemes for Computational Acoustics on Curvilinear Meshes. J. Comp. Acoustics, 9(4): 1259-1286, 2001.
31. P.D. Thomas and C.K. Lombard. Geometric conservation law and its application to flow computations on moving grids. AIAA Journal, 17(10):1030-1037, 1979.
32. R. Beam and R. Warming. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations. AIAA Journal, 16(4): 393-402, 1978.
33. T.H. Pulliam and D.S. Chaussee. A Diagonal Form of an Implicit Approximate-Factorization Algorithm. Journal of Computational Physics, 39(2):347-363, 1981.
34. Jameson, W. Schmidt, and E. Turkel. Numerical Solutions of the Euler Equations by a Finite Volume Method Using Runge-Kutta Time Stepping Schemes. AIAA Paper 81-1259, 1981.
35. T. Pulliam. Artificial Dissipation models for the Euler Equations. AIAA, 24(12):1931-1940, 1986.
36. M. R Visbal and R.E. Gordnier. A High-Order Flow Solver for Deforming and Moving Meshes. AIAA Paper 20002619, June 2000.
37. M. Visbal. Advances in high-resolution schemes for computational acoustics on general geometries. Proceedings of the Symposium on Developments in Computational Aero-and Hydro-Acoustics, Oct. 2001.
38. M.R. Visbal, D.V. Gaitonde, and S.P. Gogineni. Direct Numerical Simulation of a Forced Transitional Plane Wall Jet. AIAA Paper 98-2643, June 1998.
39. M R, Visbal and R.E. Gordnier. Direct Numerical Simulation of the Interaction of a Boundary Layer with a Flexible Panel. AIAA Paper 2001-2721, June 2001.
40. D P. Rizzetta, M. R. Visbal, and G. A. Blaisdell. Application of a High-Order Compact Difference Scheme to Large-Eddy and Direct Numerical Simulation. AIAA Paper 99-3714, June 1999.
41. R.E. Gordnier and M.R. Visbal. High-Order Compact Difference Scheme Applied to the Simulation of a Low Sweep Delta Wing Flow. AIAA Paper 2003-0620, 2003.
42. M J. Stanek and M. R. Visbal. Investigation of Vortex Development on a Pitching Slender Body of Revolution. Journal of Aircraft, 30(5):711-718, September-October 1993.
43. M R. Visbal. Computed Unsteady Structure of Spiral Vortex Breakdown on Delta Wings. AIAA-96-2074, June 1996.
44. T L. Doligalski, C. R. Smith, and J. D. A. Walker. Vortex Interactions with Walls. Annual Review of Fluid Mechanics, 26:573-616, 1994.
45. K. Visser and A.E. Washburn. Transition Behavior on Flat Plate Delta Wings. AIAA Paper 94-1850-CP, 1994.
46. S. Leibovich. Vortex Stability and Breakdown: Survey and Extension. AIAA, 22(9):1192-1206, 1984.