Unsteady separated flows over three-dimensional slender bodies

Progress in Aerospace Sciences

Volumn 40, Issue 4-5, 2004, Pages 291-320

  Zeiger, M D ^a   Telionis, D P ^b,c   Vlachos, P P ^b  

^a Aeroprobe Corporation   (United States)

^b Virginia Polytechnic Institute and State University   (United States)

^c VA Tech   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL COMPLEXITY; FLUID STRUCTURE INTERACTION; HYDRODYNAMICS; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; SWIRLING FLOW; TURBULENT FLOW; UNSTEADY FLOW; VORTEX FLOW;

COMPUTATIONAL TOOLS; SEPARATED FLOW; SLENDER BODIES; SWIRLING MOTION;

AERODYNAMICS;

EID: 4243138105     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.paerosci.2004.06.002     Document Type: Review

References (70)

1. Telionis DP. Unsteady viscous flow. Berlin: Springer; 1981.
2. Lighthill MJ. Introduction, boundary-layer theory. In: L. Rosenhead, editor. Laminar boundary layers. Oxford; 1963. p. 46-109.
3. Costis CE, Hoang NT, Telionis DP. Laminar separating flow over a prolate spheroid. J Aircr 1989;26(9):810-6.
4. Ramberg SE. The effects of yaw and finite length upon vortex wakes of stationary and vibrating circular cylinders. J Fluid Mech 1983;128:81-107.
5. Rediniotis OK, Hoang NT, Telionis DP. Multi sensor investigation of delta wing high-alpha aerodynamics. AIAA paper no 91-0735, 1991.
6. Prandtl L. Ueber Fluessigkeitsbewegung mit sehr kleiner Reibung. Third international congress of mathematics, Heidelberg, 1904. p. 484-91.
7. Williamson CHK. Vortex dynamics in the wake of a cylinder. In: Green SI, editor. Fluid vortices; 1995. p. 155-234.
8. Williamson CHK. Vortex dynamics in the cylinder wake. Annu Rev Fluid Mech 1996;477-539.
9. Hammache M, Gharib M. An experimental study of the parallel and oblique vortex shedding from circular cylinders. J Fluid Mech 1991;232:567-90.
10. Thomson KD, Morrison DF. The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidence. J Fluid Mech 1991;50(4):751-83.
11. Lament PJ, Hunt BL. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream. J Fluid Mech 1976; 76(3):519-59.
12. Lowson MV, Ponton AJC. Symmetry breaking in vortex flow on conical bodies. AIAA J 1992;30(6):1576-83.
13. Stanek MJ, Visbal MR. Investigation of vortex development on a pitching slender body of revolution. AIAA paper 91-3273-CP, 1991.
14. Poll DIA. Some observation of the transition process on the windward face of a long yawed cylinder. J Fluid Mech 1985;150:329-56.
15. Bloor MS. The transition to turbulence in the wake of a circular cylinder. J Fluid Mech 1964; 19:290-304.
16. Wei T, Smith CR. Secondary vortices in the wake of circular cylinders. J Fluid Mech 1986;169:513-33.
17. Ayoub A, Karamcheti K. An experiment on the past a finite circular cylinder at high critical and supercritical Reynolds numbers. J Fluid Mech 1982;118:1-26.
18. Okamoto T, Yagita M. The experimental investigation of the flow past a circular cylinder of finite length placed normal to the plane surface in a uniform stream. Bull JSME 1973;16:805-14.
19. Hoang NT, Telionis DP. The dynamic character of the wake of an axisymmetric body at an angle of attack. AIAA paper 91-3268, September 1991.
20. Slaouti A, Gerrard JH. An experimental investigation of the end effects on the wake of acircular cylinder towed through water at low Reynolds numbers. J Fluid Mech 1981;112:297-314.
21. Hunt BL. Asymmetric vortex forces and wakes on slender bodies. AIAA paper 82-1336, August 1982.
22. Ericsson LE, Reding JP. Steady and unsteady vortex-induced asymmetric loads on slender vehicles. J Spacecr 1981;18(2):97-109.
23. Malcolm GN. Forebody vortex control. Prog Aerosp Sci 1991:28:171-234.
24. Tobak M, Schiff LB, Peterson VL. Aerodynamics of bodies of revolution in coning motion. AIAA J 1969;7(1).
25. Keener ER. Flow-separation patterns on symmetric forebodies. NASA TM 86016, January 1986.
26. Gee K, Rizk YM, Schiff LB. Forebody tangential slot blowing on an aircraft geometry. J Aircr 1994;31(4): 922-8.
27. Degani D, Zilliac GG. Experimental study of nonsteady asymmetric. flow around an ogive-cylinder at incidence. AIAA J 1990;28(4):642-9.
28. Montividas R, Reisenthel P, Nagib H. The scaling and control of vortex geometry behind pitching cylinders. AIAA paper 89-1003, 1989.
29. Peake DJ. Owen FK, Johnson DA. Control of forebody vortex orientation to alleviate side forces. AIAA paper 80-0183, January 1980.
30. Degani D, Schiff LB. Numerical simulation of the effect of spatial disturbance on vortex asymmetry. AIAA J 1991;29(3):344-52.
31. Degani. Effect of splitter plate on unsteady flows around a body of revolution at incidence. Phys Fluids 1991;A3(9).
32. Huerre P, Monkewitz PA. Local and global instabilities in spatially developing flows. Annu Rev Fluid Mech 1990; 22:473-537.
33. Theofilis V. Advances in global linear instability analysis of nonparallel and three-dimensional flows. Prog Aerosp Sci 2003:39:249-315.
34. Zilliac GG, Degani D, Tobak M. Asymmetric vortices on a slender body of revolution. AIAA J 1991;29:667-75.
35. Moskovitz CA, Hall RM, DeJarnette FR. Effects of nose bluntness, roughness and surface perturbations on the asymmetric flow past slender bodies at large angles of attack. AIAA paper 89-2236, 1989.
36. Degani D, Tobak M. Numerical, experimental, and theoretical study of convective instability of flows over pointed bodies at incidence. AIAA paper 91-0291, January 1991.
37. Bernhardt J, Williams D. The effect of Reynolds number on control of forebody asymmetry by suction and bleed. Phys Fluids 1993;5:291-3.
38. Bernhardt J, Williams D. Proportional control of asymmetric forebody vortices. AIAA J 1998;36:2087-93.
39. Lamont PJ. Pressures around an inclined ogive cylinder with laminar, transitional, or turbulent separation. AIAA J 1982;20(11):1492-9.
40. Lamont PJ. The effects of Reynolds number on normal and side forces on ogive cylinders at high incidence. AIAA paper 85-1799.
41. Degani D. Numerical investigation of the origin of vortex asymmetry. AIAA paper 90-0593, January 1990.
42. Zeiger MD, Vlachos PP, Telionis DP. The dynamic character of a vortical flow over a slender axisymmetric body. AIAA paper 2001-1036, 2001.
43. Calarese W. An experimental study of vortex flow on a slender body at large incidence. AIAA J 1982;20(4): 477-8.
44. Hunt BL, Dexter PC. Pressure on a slender body at high angle of attack in a very low turbulence level air stream. Paper 17, AGARD conference proceedings CP-247, 1979.
45. Wardlaw AB, Yanta WJ. Multistage vortex patterns on slender, circular bodies at high incidence. AIAA J 1982;20(4):509-15.
46. Ericsson LE, Reding JP. Dynamics of forebody separation and associated vortices. J Aircr 1985;22:329-35.
47. Keener ER, Chapman GT, Cohen L, Taleghani J. Side forces on a tangent-ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7. NASA TM X-3437, February 1977.
48. Jenkins JE. Nonlinear aerodynamic characteristics of a 65 degree delta wing in rolling motion: implications to testing and flight mechanics analysis. AIAA paper 97-0742, January 1997.
49. Reisenthel PH. Development of a nonlinear indicial model for maneuvering fighter aircraft. AIAA paper 96-0896, 1996.
50. Goman M, Khrabov A. State-space representation of aerodynamic characteristics of an aircraft at high angles of attack. J Aircr 1994;31(5):1109-15.
51. Ericsson LE. Prediction of slender body coning characteristics. J Spacecr 1991;28(1):43-9.
52. Ericsson LE. Unsteady flow separation on slender bodies at high angles of attack. J Spacecr Rockets 30;6:689-95.
53. Gad-el-Hak, Ho-Chih-Ming. Unsteady flow around an ogive cylinder. J Aircr 1986;23:520-8.
54. Zeiger MD, Rediniotis OK, Donnelly MJ, Telionis DP. Temporal evolution of the flow field over a pitching tangent-ogive cylinder. AIAA paper 95-0441, January 1995.
55. Zeiger MD, Telionis DP. Vortex asymmetry over ogive cylinders in coning and pitching motions. AIAA paper 96-0206, January 1996.
56. Panzer EC, Rediniotis OK, Telionis DP. The hemisphere-cylinder in dynamic pitch-up motions. AIAA paper 93-2963, 1993.
57. Iwanski K, Nelson B. Aerodynamics of forebodies undergoing longitudinal motions. AIAA paper 99-0987, January 1999.
58. Smith LH, Nunn RH. Aerodynamic characteristics of an axisymmetric body undergoing a uniform pitching motion. J Spacecr 1976;13:8.
59. Schiff LB, Tobak M. Results from a new wind tunnel apparatus for studying coning and spinning motions of bodies of revolution. AIAA J 1970;8(11):1953-9.
60. Yoshinaga T, Tate A, Inoue K. Coning motion of slender bodies at high angles of attack in low speed flow. AIAA paper 81-1899, August 1981.
61. Ericsson LE. Unsteady flows. Tactical missile aerodynamics: general topics, progress in astronautics and aeronautics. Washington, DC: AIAA 1991;141:452-503 [chapter 11].
62. Zeiger MD, Telionis DP. Effect of coning motion and blowing on the asymmetric side forces on a slender forebody. AIAA paper 97-0549, January 1997.
63. Wetzel TG, Simpson RL. Unsteady crossflow separation location measurements on a maneuvering 6:1 prolate spheroid. AIAA J 1998;36(11):2063-71.
64. Hoang NT, Wetzel TG, Simpson RL. Unsteady measurements over a 6:1 prolate spheroid undergoing a pitch up maneuver. AIAA paper 94-0197, January 1994.
65. Kramer B, Smith B. F/A-18 and F-16 forebody vortex control, static and rotary-balance results. Fourth NASA high alpha conference, Dryden flight research center, July 1994.
66. Kramer BR, Malcolm GN, Suarez CJ, James KD. Rotary-balance and static wind tunnel tests of forebody vortex control techniques on an F/A-18. AIAA ICAS-94-3.4.3, September 1994.
67. Celik ZZ, Pedreiro N, Roberts L. Dynamic roll and yaw control by tangential forebody blowing. AIAA paper 94-1853, June 1994.
68. Cobleigh BR. High-angle-of-attack yawing moment asymmetry of the aircraft from flight test. AIAA paper 94-1005.
69. Ralston J. Examination of vortex control on a chined forebody during maneuvering flight conditions. Fourth NASA high angle-of-attack project and technology conference, Dryden flight research center, July 1994.
70. Bernhardt J, Williams D. Closed-loop control of forebody flow asymmetry. AIAA paper 95-0651, January 1995.