Aspects of vortex breakdown

Progress in Aerospace Sciences

Volumn 30, Issue 1, 1994, Pages 1-59

  Delery, Jean M ^a  

^a ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0002251012     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/0376-0421(94)90002-7     Document Type: Article

References (137)

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3. Slender delta wing at high angles of attack
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22. Measurements of vortex-breakdown position at low speed on a series of sharp-edged symmetrical models
23. Low-speed wind-tunnel experiments on a series of sharp-edged delta wings
24. Numerical simulation of the effect of variation of angle of attack and sweep angle on vortex breakdown over delta wings
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26. Experimental study on vortex and shock wave development on a 65° delta wing
27. An experimental study of the flow over a sharp-edged delta wing at subsonic and transonic speeds
28. Flow studies of slender wing vortices
29. Analytical prediction of slender wing rock
30. Observations of the flow produced in a cylindrical container by a rotating endwall
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34. Observations and LDA measurements of confined turbulent vortex
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37. An experimental map of the internal structure of a vortex breakdown
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53. Experimental investigation of the transonic flow at the leeward side of a delta wing at high incidence
54. On the hydrodynamic and hydromagnetic stability of swirling flows
55. Untersuchungen über das Aufplatzen der Wirbel an schlanken Deltaflügeln
56. Vortex breakdown effects on the low-speed aerodynamic characteristics of slender delta wings in symmetrical flow
57. Turbulence in low altitude fireball
58. On the vortex breakdown phenomenon in a swirling pipe-flow
59. Numerical solutions of Navier-Stokes equations for the structure of a trailing vortex
60. Airfoil pressure measurements during oblique shock wave-vortex interaction in a Mach 3 stream
61. Computation of steady and unsteady compressible quasi-axisymmetric vortex flow and breakdown
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63. The effect of small blowing on vortex breakdown of a swirling flow
64. Effects of leading edge shape and vortex burst on the flowfield of a 70-degree-sweep delta wing
65. The flowfield of bursting vortices over moderately swept delta wings
66. Detailed flowfield measurements over a 75° swept delta wing for code validation
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71. Détermination de critéres d'éclatement par résolution des équations d'Euler et de Navier-Stokes
72. Séparation de l'écoulement laminaire tridimensionnel
73. Lignes de courant d'un écoulement permanent
74. Remarques sur l'éclatement axisymétrique d'un tourbillon
75. The structure of vortex breakdown
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90. Numerical simulation of a three-dimensional vortex breakdown
91. An experimental study of shock wave/vortex interaction
92. Etude expérimentale de l'éclatement tourbillonnaire sur aile delta en écoulement incompressible
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100. Etude expérimentale de l'éclatement d'un tourbillon engendré par une aile delta
101. Vortex breakdown induced by an adverse pressure gradient: experimental and numerical approaches
102. Etude numérique de l'éclatement de tourbillons soumis á des gradients de pression
103. The effects of a contoured apex on vortex breakdown
104. Contribution á l'étude d'un écoulement tourbillonnaire en fluide incompressible
105. Visualization and flow surveys of the leading edge vortex structure on delta wing planforms
106. Preliminary results of low speed wind tunnel tests on a gothic wing of aspect ratio 1.0
107. Hypersustentation et équilibrage des ailes élancées
108. Vortex development and breakdown
109. The critical state: a trapped wave model of vortex breakdown
110. Forced and periodic vortex breakdown
111. On stationary and travelling vortex breakdowns
112. Vortex Breakdown in Swirling Conical Flows
113. Effect of the adverse pressure gradient on vortex breakdown
114. On the units of cubic and bicubic fields
115. Laser velocimetry measurements of supersonic vortex flows on a simple razor-edged delta wing
116. Etude expérimentale et théorique de la turbulence dans les écoulements décollés
117. Etudes expérimentales d'écoulements tourbillonnaires soumis á des effets de gradient de pression adverse
118. Etude expérimentale des conditions d'éclatement d'un tourbillon d'aile delta
119. Contribution de la visualisation á l'étude instationnaire de l'éclatement tourbillonnaire
120. Etude expérimentale de l'écoulement á l'extrados d'une aile delta en régime incompressible
121. A criterion for vortex breakdown
122. Analysis of the vortex breakdown phenomenon. Part 1
123. The inner viscous solution for the core of a leading-edge vortex
124. A critical review of vortex-breakdown theory
125. Vortex breakdown phenomena in a circular pipe (1st Report, Modes of Stationary Breakdown)
126. Vortex breakdown phenomena in a circular pipe (2nd Report, Flow Modes of Unsteady Type Breakdowns)
127. Multigrid method for a vortex breakdown simulation
128. Numerical study of axisymmetric vortex breakdowns
129. An experimental investigation of the effect of adverse pressure gradient on vortex breakdown
130. Examination of group velocity criterion for breakdown of vortex flow in a divergent duct
131. Experiments on the axisymmetric vortex breakdown in a swirling air flow
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134. Quelques résultats expérimentaux sur les ailes en fléches, aux faibles vitesses, obtenus en tunnel hydrodynamique
135. Sur l'éclatement des tourbillons
136. Bulbes de recirculation au sein d'un sillage