Plasma-Based Control of Transition on a Wing with Leading-Edge Excrescence (English)
- New search for: Rizzetta, Donald P
- New search for: Rizzetta, Donald P
- New search for: Visbal, Miguel R
In:
AIAA journal
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54
, 1
; 129-140
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2016
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ISSN:
- Article (Journal) / Print
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Title:Plasma-Based Control of Transition on a Wing with Leading-Edge Excrescence
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Contributors:Rizzetta, Donald P ( author ) / Visbal, Miguel R
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Published in:AIAA journal ; 54, 1 ; 129-140
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Publisher:
- New search for: AIAA
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Place of publication:Reston, Va. [u.a.]
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Publication date:2016
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ISSN:
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ZDBID:
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DOI:
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Type of media:Article (Journal)
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Type of material:Print
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Language:English
- New search for: 770/7040
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Keywords:
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Table of contents – Volume 54, Issue 1
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Announcements, Comments, and Acknowledgments| 2016
- 12
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AIAA Policy Statements and Manuscript Review Process| 2016
- 17
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Generalized Formulation and Review of Piston Theory for AirfoilsMeijer, Marius-Corné / Dala, Laurent et al. | 2015
- 28
-
Unstart of a Hypersonic Inlet with Side Compression Caused by Downstream ChokingZhang, Q. F. / Tan, H. J. / Sun, S. / Bu, H. X. / Rao, C. Y. et al. | 2015
- 39
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Control of Crossflow Transition at High Reynolds Numbers Using Discrete Roughness ElementsLi, Fei / Choudhari, Meelan / Carpenter, Mark / Malik, Mujeeb / Chang, Chau-Lyan / Streett, Craig et al. | 2015
- 53
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Numerical Simulations of Transition due to Isolated Roughness Elements at Mach 6Van den Eynde, Jeroen P. J. P. / Sandham, Neil D. et al. | 2015
- 66
-
Impact of Deep Gaps on Laminar–Turbulent Transition in Compressible Boundary-Layer FlowZahn, Johannes / Rist, Ulrich et al. | 2015
- 77
-
Compact Disturbance Equations for Aeroacoustic SimulationsDu, Yongle / Morris, Philip J. et al. | 2015
- 88
-
Exergy-Based Performance Assessment of the NASA Common Research ModelArntz, Aurélien / Hue, David et al. | 2015
- 101
-
Validation of a High-Order Large-Eddy Simulation Solver Using a Vertical-Axis Wind TurbineKanner, Samuel / Persson, Per-Olof et al. | 2015
- 113
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Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model WingKenway, Gaetan K. W. / Martins, Joaquim R. R. A. et al. | 2015
- 129
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Plasma-Based Control of Transition on a Wing with Leading-Edge ExcrescenceRizzetta, Donald P. / Visbal, Miguel R. et al. | 2015
- 141
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Flow Control over an Airfoil in Fully Reversed Condition Using Plasma ActuatorsClifford, Chris / Singhal, Achal / Samimy, Mo et al. | 2015
- 150
-
Aerodynamic Analysis of Projectiles in Ground Effect at Near-Sonic Mach NumbersDoig, Graham / Wang, Shibo / Kleine, Harald / Young, John et al. | 2015
- 161
-
Injection into Supersonic Boundary LayersSchmidt, B. E. / Bitter, N. P. / Hornung, H. G. / Shepherd, J. E. et al. | 2015
- 174
-
Frequency-Response Characteristics of Polymer/Ceramic Pressure-Sensitive PaintPandey, Anshuman / Gregory, James W. et al. | 2015
- 186
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Decoupled Multidisciplinary Design Optimization Formulation for Interdisciplinary Coupling Satisfaction Under UncertaintyBrevault, Loïc / Balesdent, Mathieu / Bérend, Nicolas / Le Riche, Rodolphe et al. | 2015
- 206
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Measuring Surface Pressures on Rotor Blades Using Pressure-Sensitive PaintWatkins, A. Neal / Leighty, Bradley D. / Lipford, William E. / Goodman, Kyle Z. / Crafton, Jim / Gregory, James W. et al. | 2015
- 216
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Coriolis Effect on Dynamic Stall in a Vertical Axis Wind TurbineTsai, Hsieh-Chen / Colonius, Tim et al. | 2015
- 227
-
Accurate Response of Wing Structures to Free-Vibration, Load Factors, and Nonstructural MassesCarrera, Erasmo / Pagani, Alfonso et al. | 2015
- 242
-
Experimental Study on Open Rotor Noise Shielding by Hybrid-Wing-Body AircraftGuo, Yueping / Thomas, Russell H. et al. | 2015
- 254
-
Coalescence in the Sound Field of a Laboratory-Scale Supersonic JetFiévet, Romain / Tinney, Charles E. / Baars, Woutijn J. / Hamilton, Mark F. et al. | 2015
- 266
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Efficient Mode Matching Based on Closed-Form Integrals of Pridmore-Brown ModesOppeneer, M. / Rienstra, S. W. / Sijtsma, P. et al. | 2015
- 280
-
Carrera Unified Formulation for Free-Vibration Analysis of Aircraft StructuresCarrera, Erasmo / Zappino, Enrico et al. | 2015
- 293
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Trim and Structural Optimization of Subsonic Transport Wings Using Nonconventional Aeroelastic TailoringStanford, Bret K. / Jutte, Christine V. / Wieseman, Carol D. et al. | 2015
- 310
-
General Three-Dimensional Relation for Oblique Shocks on Swept RampsDomel, Neal D. et al. | 2015
- 320
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Complex Geometry Effects on Cavity ResonanceCasper, Katya M. / Wagner, Justin L. / Beresh, Steven J. / Henfling, John F. / Spillers, Russell W. / Pruett, Brian O. M. et al. | 2015
- 331
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Unstructured Mesh Manipulation in Response to Surface DeformationMasters, James S. / Tatum, Kenneth E. et al. | 2015
- 343
-
Prediction of Scattered Broadband Shock-Associated NoiseMiller, Steven A. E. et al. | 2015
- 360
-
Effect of Ballonet Sloshing on the Stability Characteristics of an Airship (TN)Wang, X.-l. et al. | 2016
- 360
-
Effect of Ballonet Sloshing on the Stability Characteristics of an AirshipWang, Xiao-liang et al. | 2015
- 364
-
Far Field Predicted by Piston TheoryDowell, Earl H. et al. | 2015
- 364
-
Far Field Predicted by Piston Theory (TN)Dowell, E. H. et al. | 2016
- 366
-
Development of Reduced Unsteady Vortex Lattice Method Using Proper Orthogonal Decomposition Technique (TN)Cao, B. et al. | 2016
- 366
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Development of Reduced Unsteady Vortex Lattice Method Using Proper Orthogonal Decomposition TechniqueCao, Bochao et al. | 2015
- 1172
-
Passive Flexibility Effect on Oscillating Foil Energy HarvesterLiu, Wendi et al. | 2016
- 1235
-
Partial-Burning Regime for Quasi-Steady Droplet Combustion Supported by Cool FlamesNayagam, Vedha et al. | 2016
- 1250
-
Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender ConeCasper, Katya M et al. | 2016
- 1264
-
Kinetic Models and Gas-Kinetic Schemes for Hybrid Simulation of Partially Rarefied FlowsColonia, S et al. | 2016
- 1277
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Development of Magnetic Suspension and Balance System for Intermittent Supersonic Wind TunnelsTakagi, Yoshiki et al. | 2016
- 1350
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Efficient Optimization of Cylindrical Stiffened Shells with Reinforced Cutouts by Curvilinear StiffenersHao, P et al. | 2016
- 1364
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Formation of Leading Vortex Pair in Two-Dimensional Starting JetsGao, Lei et al. | 2016
- 1370
-
Well-Balanced, Conservative Finite Difference Algorithm for Atmospheric FlowsGhosh, Debojyoti et al. | 2016
- 1394
-
Combined Structural and Control Optimum Design of Fuzzy Composite StructuresRao, Singiresu S et al. | 2016
- 1403
-
Mechanism and Prediction for Occurrence of Shock-Train Sharp Forward MovementXu, Kejing et al. | 2016
- 1472
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Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting WedgesXiang, G. X et al. | 2016
- 1482
-
Large-Eddy Simulation of Supersonic Round Jets: Effects of Reynolds and Mach NumbersBellan, Josette et al. | 2016
- 1499
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Two-Zone Model for Predicting the Trajectory of Liquid Jet in Gaseous CrossflowBroumand, Mohsen et al. | 2016
- 1603
-
Modeling Internal Flow Through a Rotating Duct Using Quasi 1-D Euler EquationsKarpatne, Anand et al. | 2016
- 1616
-
Large Low-Frequency Oscillations Initiated by Flow Control on a Poststall AirfoilBernardini, Chiara et al. | 2016
- 1628
-
Streamwise Oscillation of Airfoils into Reverse FlowGranlund, Kenneth O et al. | 2016
- 1693
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Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 RocketsBetti, Barbara et al. | 2016
- 2645
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Performance of a Newton–Krylov–Schur Algorithm for Solving Steady Turbulent FlowsBrown, David A et al. | 2016