Some compressibility effects on the lee side flow structures of cruciform wing-body configurations with very low aspect ratio wings

Aerospace Science and Technology

Volumn 29, Issue 1, 2013, Pages 373-385

  Tuling, S ^a   Dala, L ^b   Toomer, C ^c  

^a DSI CSIR Nanotechnology Innovation Centre   (South Africa)

^b UNIVERSITY OF THE WITWATERSRAND   (South Africa)

^c UNIVERSITY OF THE WEST OF ENGLAND   (United Kingdom)

Author keywords

Symmetric vortices; Vortex shedding Slender bodies Very low aspect ratio wings

Indexed keywords

ACCELERATED FLOWS; COMPRESSIBILITY EFFECTS; CROSSFLOW VELOCITIES; RECIRCULATION REGIONS; SLENDER BODIES; SYMMETRIC VORTEX; VERY LOW ASPECT RATIOS; WING-BODY CONFIGURATIONS;

ASPECT RATIO; LOW ASPECT RATIO WINGS; MACH NUMBER; VORTEX FLOW; VORTEX SHEDDING;

AERODYNAMICS;

EID: 84880916424     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2013.04.008     Document Type: Article

References (36)

1. S.B. Angelucci A multi-vortex method for axisymmetric bodies at angle of attack J. Aircr. 12 1971 959 966
2. A.E. Bryson Symmetric vortex separation on circular cylinders and cones Appl. Mech. 26 1959 643 648
3. J. Cai, F. Liu, and S. Lou Stability of symmetric vortices in two dimensions and over three-dimensional slender conical bodies J. Fluid Mech. 480 2003 65 94
4. J. Cai, H. Tsai, S. Lou, and F. Liu Stability of vortex pairs over slender conical bodies: Analysis and numerical computation AIAA J. 46 3 2003 712 722
5. C. Cerretelli, and C.H.K. Williamson A physical mechanism for vortex merging J. Fluid Mech. 475 2003 41 77
6. M.S. Chong, A.E. Perry, and B.J. Cantwell A general classification of three-dimensional flow fields Phys. Fluids A, Fluid Dyn. 2 1990 765 777
7. D. Degani Effect of splitter plate on unsteady flows around a body of revolution at incidence Phys. Fluids A, Fluid Dyn. 3 1991 2122 2131
8. D. Degani Numerical simulation of vortex unsteadiness on a slender body at high incidence AIAA J. 30 3 1992 841 843
9. D. Degani, and L.B. Schiff Numerical simulation of the effect of spatial disturbances on vortex asymmetry AIAA J. 29 3 1991 344 352
10. D. Degani, M. Tobak, Numerical, experimental, and theoretical study of convective instability of flows over pointed bodies at incidence, AIAA-91-0291.
11. D. Degani, and G.G. Zilliac Experimental study of nonsteady asymmetric flow around an ogive-cylinder at incidence J. Spacecr. Rockets 28 4 1990 629 642
12. L.E. Ericsson, and J.P. Reading Asymmetric vortex shedding from bodies of revolution Tactical Missile Aerodynamics 1986 American Institute of Aeronautics and Astronautics 243 298
13. L.E. Ericsson Prediction of slender body coning characteristics J. Spacecr. Rockets 28 1 1991 43 49
14. Gad-el-Hak, and Ho-Chih-Ming Unsteady flow around an ogive cylinder J. Aircr. 23 1986 520 528
15. B.L. Hunt, Asymmetric vortex forces and wakes on slender bodies, AIAA-82-1336.
16. J.C.R. Hunt, A.A. Wray, and P. Moin Eddies, streams, convergence zones in turbulent flows Proceedings of the Summer Program 1988, CTR-S88 1988 193 207
17. K. Iwanski, B. Nelson, Aerodynamics of forebodies under-going longitudinal motions, AIAA-99-0987.
18. J. Jeong, and F. Hussain On the identification of a vortex J. Fluid Mech. 285 1995 69 94
19. L.H. Jorgensen, Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack, NASA-TR-474 formerly issued as NASA-TM-X-73,123 with limited distribution, September 1977.
20. L.H. Jorgensen, and E.W. Perkins Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2 NACA Report 1371 1958
21. P.J. Lamont, Pressure measurements on an ogive-cylinder at high angles of attack with laminar, transitional, or turbulent separation, AIAA 80-1556, August 1980.
22. J.M. Macha Drag of circular cylinders at transonic Mach numbers J. Aircr. 16 6 1977 605 607
23. J.F. Marshall, F.D. Deffenbaugh, Separated flow over bodies of revolution using an unsteady discrete-vorticity wake, NASA CR-2414, June 1974.
24. J.R. Mello Investigation of normal-force distributions and wake vortex characteristics of bodies of revolution at supersonic speeds J. Aeronaut. Sci. 3 1959 155 168
25. M.R. Mendenhall, S.C. Perkins Jr., Predicted vortex shedding from circular and noncircular bodies in supersonic flow, NASA CR-3754, January 1984.
26. T. Sarpkaya, An inviscid model of two-dimensional vortex shedding for transient and asymptotically steady separated flow over a cylinder, AIAA-79-0281, January 1979.
27. G.M. Simpson, T.J. Birch, Some aerodynamic characteristics of missiles having very low aspect ratio wings, AIAA 2001-2410, 2001.
28. K.D. Thomson, and D.F. Morrison The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidence J. Fluid Mech. 50 4 1971 751 783
29. B.E. Tinling, C.Q. Allen, An investigation of the normal-force and vortex-wake characteristics of an ogive-cylinder body at subsonic speeds, NASA TN D-1297, April 1962.
30. S. Tuling, L. Dala, and C. Toomer Lee side flow structures of very low aspect ratio cruciform wing-body configurations J. Spacecr. Rockets 2013 in press, manuscript ID 2012-10-A32522.R1
31. G. Wang, and X.-G. Liang Development and evolution of flow over three-dimensional cylinder Chin. Phys. 14 7 2005 1392 1405
32. A.B. Wardlaw, Prediction of normal force, pitching moment and yawing force on bodies of revolution at angles of attack up to 50 degrees using a concentrated vortex flowfield model, NOLTR 73-209, October 1973.
33. A.B. Wardlaw, Multivortex model of asymmetric shedding on slender bodies at high angle of attack, AIAA 75-123, January 1975.
34. H. Werle, Tourbillons de corps fuseles aux incidences elevees, ONERA Tech. Note No. 175, 1971.
35. M.D. Zeiger, D.P. Telionis, Vortex asymmetry over ogive cylinders in coning and pitching motions, AIAA-96-0206.
36. M.D. Zeiger, D.P. Telionis, and P.P. Vlachos Unsteady separated flows over three-dimensional slender bodies Prog. Aerosp. Sci. 40 2004 291 320