Research into vortex breakdown control

Progress in Aerospace Sciences

Volumn 37, Issue 4, 2001, Pages 385-418

  Mitchell, Anthony M ^a   Délery, Jean ^b  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK INDICATORS; DELTA WING AIRCRAFT; OSCILLATIONS; PNEUMATICS;

VORTEX BREAKDOWN;

VORTEX FLOW;

EID: 0035328405     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0376-0421(01)00010-0     Document Type: Review

References (97)

1. Quelques résultats expérimentaux sur les ailes en flèche, aux faibles vitesses, obtenus en tunnel hydrodynamique
2. Some developments in the theory of vortex breakdown
3. On stationary and traveling vortex breakdowns
4. Aspects of vortex breakdown
5. Sur l'éclatement des tourbillons d'apex d'une aile delta aux faibles vitesses
6. Robert legendre, Henri Werlé: Toward the elucidation of three-dimensional separation
7. Separation control by trapped vortices
8. Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience
9. Analysis and design of strake-wing configuration
10. Analysis of strake vortex breakdown characteristics in relation to design features
11. Leading-edge 'Vortex Flaps' for enhanced subsonic aerodynamics of slender wings
12. Effectiveness of leading-edge vortex flaps on 60 and 70 degree delta wings
13. The aerodynamics of inverted leading-edge flaps on delta wings
14. Trailing edge flap influences on leading edge vortex flap aerodynamics
15. The impact of strakes on a vortex-flapped delta wing
16. Experimental and computations studies of a delta wing apex-flap
17. Flow control over delta wings at high angles of attack
18. Investigation of the "Tabbed" vortex flap
19. Experimental investigation of apex fence flaps on delta wings
20. Controlling of delta wing leading-edge vortex with cavity flaps
21. Control of transient development of leading-edge vortices by vortex cavity flaps
22. Experimental study of vortex flow control on double-delta wings using fillets
23. Unsteady aerodynamic effects of trailing edge controls on delta wings
24. Control of vortex breakdown with leading-edge devices
25. Active control of vortex breakdown over a delta wing
26. Active control of vortex lift at high angles of attack
27. Multiple-actuator control of vortex breakdown on a pitching delta wing
28. Effect of leading-edge flaps on vortices and vortex breakdown
29. Zur umstronmung scharfkantiger schlanker deltaflugel bei grossen anstellwinkeln
30. Lift augmentation by lateral blowing over a lifting surface
31. High lift applications of spanwise blowing
32. Vortex flows
33. Transient response of leading-edge vortices to localized suction
34. Vortex suppression on highly-swept wings by suction boundary-layer control
35. Effect of shear-layer control on leading-edge vortices
36. The effects of leading-edge suction on delta wing vortex breakdown
37. Visualisation hydrodynamique de l'écoulement à basse vitesse autour d'une maquette d'avion du type 'Concorde'
38. Effects of trailing-edge jet entrainment on delta wing vortices
39. Differential and vectored trailing-edge jet control of delta wing vortices
40. Trailing-edge jet control of leading edge vortices of a delta wing
41. Multiple-actuator control of vortex breakdown on a pitching delta wing
42. Vortex breakdown on pitching delta wing: Control by intermittent trailing-edge blowing
43. Control of leading-edge vortex breakdown by trailing-edge injection
44. Experiments on a delta wing using leading-edge blowing to remove secondary separation
45. Exploratory investigation of the effects of blowing from the leading-edge of a delta wing
46. Lift augmentation by lateral blowing over a lifting surface
47. High lift applications of spanwise blowing
48. Contrôle du décollement d'une surface portante par un jet transversal
49. Flow characteristics about a delta wing at 15° incidence with and without edge blowing
50. A conceptual study of leading-edge-vortex enhancement by blowing
51. Leading-edge vortex augmentation in compressible flow
52. Augmentation of vortex lift by spanwise blowing
53. Benefits of spanwise blowing at transonic speeds
54. Effects of spanwise blowing on the aerodynamic characteristics of the F-5E
55. Effects of spanwise blowing on pressure distribution and leading-edge vortex stability
56. Effects of spanwise blowing on two fighter configurations
57. Vortex breakdown and control experiments in the Ames-Dryden water tunnel
58. An investigation of leading-edge vortices on delta wings with jet blowing
59. Control of leading edge vortex breakdown by blowing
60. Control of vortical lift on delta wings by tangential leading-edge blowing
61. Dynamic control of vortical flow on delta wings at high angles of attack
62. An experimental investigation of delta wing vortex flow with and without external jet blowing
63. Three-dimensional vortex development, breakdown and control
64. Etude expérimentale et simulation numérique de l'éclatement d'un tourbillon d'ailettes
65. Etudes fondamentales sur l'éclatement tourbillonnaire et son contrôle
66. Etude des nappes tourbillonnaires sur une aile delta de 70 degrés de flèche a 27 degrés d'incidence. Contrôle de l'éclatement par soufflage, Soufflerie F2
67. The effects of blowing on delta wing vortices during dynamic pitching at high angles of attack
68. Delta wing vortex manipulation using pulsed and steady blowing during ramp-pitching
69. Effects of leading-edge lateral blowing on delta wing aerodynamics
70. Evolution of vortical structure over delta wing with transient along-core blowing
71. Unsteady vortex structure over delta-wing subject to transient along core blowing
72. Disrupted states of vortex flow and vortex breakdown
73. Delay of vortex breakdown over a delta wing via near-core blowing
74. Oscillation of vortex breakdown location and control of the time-averaged location by blowing
75. Control of vortex breakdown location by symmetric and asymmetric blowing
76. Control of vortex breakdown by along-the-core blowing
77. Control of the discrete vortices from a delta wind
78. Control of leading edge vortices on a delta wing
79. Control of vortices on a delta wing by leading-edge injection
80. Control of vortex breakdown on a delta wing by periodic blowing and suction
81. Pressure measurements and flow field visualization on a delta wing with periodic blowing and suction
82. Velocity measurements on a delta wing with periodic blowing and suction
83. Parametric investigation of the effects of active flow control on the normal force of a delta wing
84. Numerical simulation of periodic suction and blowing control of vortex breakdown on a delta wing
85. An analysis of a pitching delta wing using high resolution pressure measurements
86. An analysis of high resolution pressure signals on a pitching delta wing