353 results on '"Miguel R. Visbal"'
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52. Plasma-Based Control of Excrescence-Generated Transition on a Swept Wing
53. Effect of compressibility on plasma-based transition control for a wing with leading-edge excrescence
54. Examination of Pitch-Plunge Equivalence for Dynamic Stall over Swept Finite Wings
55. Investigation of Transition Delay by Dynamic Surface Deformation
56. Correction: Numerical Simulation of Transonic and Supersonic Flow Over a Wall-Mounted Hemisphere
57. Further Investigation on the Effect of Sweep on Parallel Vortical-Gust/Wing Interactions on a Finite Aspect-Ratio Wing
58. Dynamic Stall of a Swept Finite Wing for a Range of Reduced Frequencies
59. Comparison of Pitch versus Plunge Maneuvers of a Finite Wing
60. Numerical Simulation of Transonic and Supersonic Flow Over a Wall-Mounted Hemisphere
61. Features of panel flutter response to shock boundary layer interactions
62. Simulation of Laminar-Flow Compatible High-Lift Wing Configuration with Flow Control
63. On the effects of vertical offset and core structure in streamwise-oriented vortex–wing interactions
64. Model reduction and analysis of deep dynamic stall on a plunging airfoil
65. Numerical Investigation of Flow Control for a Flat-Window Cylindrical Turret
66. Computational Investigation of the Effect of Sweep on Parallel Vortical-Gust/Wing Interactions
67. On the Characteristics of Three-Dimensional Dynamic Tip Stall on a Swept Wing
68. Numerical Investigation of Transition Delay by Dynamic Surface Deformation
69. Mitigation of Laminar Separation Flutter Using Plasma-Based Actuators
70. Challenges and Perspectives on CFD and Experimental Interactions for Complex Unsteady Flows
71. Evaluation of Thermoacoustic-based Forcing for Control of Dynamic Stall
72. Investigation of Inflow Turbulence Generation Method for Large Eddy Simulation of Large Domains
73. Plasma-Based Flow Control for Delay of Excrescence-Generated Transition
74. Interactions of a streamwise-oriented vortex with a finite wing
75. High-frequency forcing to mitigate unsteady separation from a bursting separation bubble
76. Understanding Abrupt Leading Edge Separation as a Mechanism for the Onset of Dynamic Stall
77. An Investigation of the Aerodynamics of a Harmonically-Pitching Airfoil in Uniform-Shear Approach Flow
78. An Overset-Mesh Approach for Wall-Modeled LES of High-Reynolds Number Airfoil Flow
79. Parametric study of supersonic flow over a wall-mounted hemisphere
80. Computational Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing
81. Further Investigations of Vortical Gust/Airfoil Interactions at a Transitional Reynolds Number
82. A study of the effect of step excrescences and free-stream disturbances on boundary layer stability
83. Lift on a steady 2-D symmetric airfoil in viscous uniform shear flow
84. Investigation of shock wave-boundary-layer interaction for flow over a wall-mounter hemisphere
85. On Ladder-Type Structure of Acoustic Tones Radiated by Transitional Airfoils
86. Control of Dynamic Stall Over a Pitching Finite-Aspect-Ratio Wing
87. Simulations of Supersonic Flow over a Wall-Mounted Cylinder Using OVERFLOW with ILES
88. High-Frequency Forcing to Delay Dynamic Stall at Relevant Reynolds Number
89. Interactions of a Trailing Vortex with a Downstream NACA0012 Wing
90. Airfoil Thickness Effects on Dynamic Stall Onset
91. An Overset-Mesh Approach for Large-Eddy Simulation of High-Reynolds Number Airfoil Flow
92. Study of the Effect of Two-dimensional Wall Non-uniformities on High-speed Boundary Layers
93. Unsteady flow structure and loading of a pitching low-aspect-ratio wing
94. Viscous and inviscid interactions of an oblique shock with a flexible panel
95. Dynamics of revolving wings for various aspect ratios
96. Stiffness effects on laminar separation flutter
97. Spatially Developing Supersonic Turbulent Boundary Layer with a Body-Force-Based Method
98. Three-dimensional vortex formation on a heaving low-aspect-ratio wing: Computations and experiments
99. Self-Sustained Pitch-Heave Oscillations and Gust Response of an Airfoil at Transitional Reynolds Numbers
100. Computational Study of Supersonic Flow Past Wall-Mounted Cylindrical Bodies
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