Seventh IUTAM Symposium on Laminar-Turbulent Transition (eBook)

Proceedings of the Seventh IUTAM Symposium on Laminar-Turbulent Transition, Stockholm, Sweden, 2009
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2010 | 2010
XXIV, 608 Seiten
Springer Netherland (Verlag)
978-90-481-3723-7 (ISBN)

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The origins of turbulent ?ow and the transition from laminar to turbulent ?ow are the most important unsolved problems of ?uid mechanics and aerodynamics. - sides being a fundamental question of ?uid mechanics, there are numerous app- cations relying on information regarding transition location and the details of the subsequent turbulent ?ow. For example, the control of transition to turbulence is - pecially important in (1) skin-friction reduction of energy ef?cient aircraft, (2) the performance of heat exchangers and diffusers, (3) propulsion requirements for - personic aircraft, and (4) separation control. While considerable progress has been made in the science of laminar to turbulent transition over the last 30 years, the c- tinuing increase in computer power as well as new theoretical developments are now revolutionizing the area. It is now starting to be possible to move from simple 1D eigenvalue problems in canonical ?ows to global modes in complex ?ows, all - companied by accurate large-scale direct numerical simulations (DNS). Here, novel experimental techniques such as modern particle image velocimetry (PIV) also have an important role. Theoretically the in?uence of non-normality on the stability and transition is gaining importance, in particular for complex ?ows. At the same time the enigma of transition in the oldest ?ow investigated, Reynolds pipe ?ow tran- tion experiment, is regaining attention. Ideas from dynamical systems together with DNS and experiments are here giving us new insights.
The origins of turbulent ?ow and the transition from laminar to turbulent ?ow are the most important unsolved problems of ?uid mechanics and aerodynamics. - sides being a fundamental question of ?uid mechanics, there are numerous app- cations relying on information regarding transition location and the details of the subsequent turbulent ?ow. For example, the control of transition to turbulence is - pecially important in (1) skin-friction reduction of energy ef?cient aircraft, (2) the performance of heat exchangers and diffusers, (3) propulsion requirements for - personic aircraft, and (4) separation control. While considerable progress has been made in the science of laminar to turbulent transition over the last 30 years, the c- tinuing increase in computer power as well as new theoretical developments are now revolutionizing the area. It is now starting to be possible to move from simple 1D eigenvalue problems in canonical ?ows to global modes in complex ?ows, all - companied by accurate large-scale direct numerical simulations (DNS). Here, novel experimental techniques such as modern particle image velocimetry (PIV) also have an important role. Theoretically the in?uence of non-normality on the stability and transition is gaining importance, in particular for complex ?ows. At the same time the enigma of transition in the oldest ?ow investigated, Reynolds pipe ?ow tran- tion experiment, is regaining attention. Ideas from dynamical systems together with DNS and experiments are here giving us new insights.

186838_1_En_BookFrontmatter_OnlinePDF.pdf 1
Seventh IUTAMSymposium on Laminar-Turbulent Transition 3
Contents 5
Preface 14
186838_1_En_1_Chapter_OnlinePDF.pdf 25
A Gradient-based Optimization Method for Natural Laminar Flow Design 25
1 Introduction 25
2 Governing equations 26
3 Optimization problem 27
4 Results 28
5 Conclusions 31
References 32
186838_1_En_2_Chapter_OnlinePDF.pdf 33
A Thermodynamic Lower Bound on Transition-Triggering Disturbances 33
1 Oscillators versus Amplifiers 33
1.1 Receptivity 33
1.2 Can transition be indefinitely delayed? 34
2 Fluctuation theory 34
2.1 One-dimensional: Langevin 34
2.1.1 Fluctuation-dissipation relationship in the frequency domain 35
2.1.2 Fluctuation-dissipation relationship in the time domain 36
2.2 Multi-dimensional fluctuation theory: Onsager 36
2.3 Infinite-dimensional fluctuation theory: Landau-Lifschitz 37
2.3.1 Fluctuations in macroscopic motion 38
3 Boundary-layer receptivity to thermodynamic fluctuations 38
3.1 The spatial stability problem 39
4 Conclusions 40
References 40
186838_1_En_3_Chapter_OnlinePDF.pdf 41
Hypersonic boundary layer transition and control 41
1 Experiments on nonlinear instability of hypersonic boundary layers at moderate Mach numbers 41
1.1 Experimental equipment 42
1.2 Statistical and bispectral analysis 42
1.3 Experimental results 42
2 Active control of hypersonic shock layer instability: direct numerical simulation and experiments 45
2.1 Experimental equipment and diagnostic methods 45
2.2 Numerical simulation 46
2.3 Results 46
References 48
186838_1_En_4_Chapter_OnlinePDF.pdf 49
Instabilities of Miscible Interfaces 49
1 Miscible core-annular flows 49
2 Miscible Hele-Shaw displacements 50
3 Miscible porous media displacements 53
References 55
186838_1_En_5_Chapter_OnlinePDF.pdf 57
Large-eddy simulations of relaminarization due to freestream acceleration 57
1 Introduction 57
2 Problem formulation 58
3 Results and discussion 59
4 Conclusions 63
References 64
186838_1_En_6_Chapter_OnlinePDF.pdf 65
Reduced-order models for flow control: balanced models and Koopman modes 65
1 Introduction 65
2 Model reduction techniques 66
2.1 Proper Orthogonal Decomposition and its limitations 66
2.2 Balanced models 67
3 Spectral analysis of nonlinear flows 67
3.1 Koopman operator and Koopman modes 68
3.2 Properties of Koopman modes and eigenvalues 69
3.3 Computing Koopman modes from snapshots 69
3.4 Example: jet in crossflow 70
3.5 Comparison with linear global modes and POD modes 71
References 72
186838_1_En_7_Chapter_OnlinePDF.pdf 73
The description of fluid behavior by coherent structures 73
1 Introduction and motivation 73
2 Global stability analysis of compressible flow about a swept parabolic body 74
3 Microlocal stability analysis of swept attachment-line boundary layer flow 75
4 Dynamic mode analysis of the wake behind a flexible membrane 77
5 Summary and conclusions 79
References 80
186838_1_En_8_Chapter_OnlinePDF.pdf 81
Instability of uniform turbulent plane Couette flow: spectra, probability distribution functions and K m closure model 81
1 Turbulent-laminar bands 81
2 Analysis of Fourier spectra 83
3 Stability analysis of K m Model 85
References 87
186838_1_En_9_Chapter_OnlinePDF.pdf 90
Sensitivity to base-flow variation of a streamwise corner flow 90
1 Introduction 90
2 Temporal asymptotic linear stability. 91
3 Sensitivity analysis 93
3.1 Sensitivity functions 93
3.2 Optimal deviation and physical mechanism 93
4 Conclusion 95
References 95
186838_1_En_10_Chapter_OnlinePDF.pdf 96
Transition Control Testing in the Supersonic S2MAWind Tunnel (SUPERTRAC project) 96
1 Introduction 96
2 Wing Definition 97
3 Control by Micron-Sized Roughness elements (MSR) 97
4 Control of the leading edge contamination (ACD) 99
5 Conclusion 101
6 Acknowledgements 101
References 101
186838_1_En_11_Chapter_OnlinePDF.pdf 102
Breakdown of Low-Speed Streaks under High-Intensity Background Turbulence 102
1 Introduction 102
2 Experimental setup and procedure 103
3 Results and discussion 104
4 Conclusions 107
References 107
186838_1_En_12_Chapter_OnlinePDF.pdf 108
Numerical Study on Transition of a Channel Flow with LongitudinalWall-oscillation 108
1 Introduction 108
2 Numerical Analysis 109
2.1 Model Flow 109
2.2 Results 110
3 Linear Stability Analysis 111
3.1 Quaisi steady analysis 111
3.2 Results 112
4 Conclusion 113
References 113
186838_1_En_13_Chapter_OnlinePDF.pdf 114
Direct Numerical Simulation of the Mixing Layer past Serrated Nozzle Ends 114
1 Introduction and Numerical Method 114
2 Results 115
3 Conclusions 119
References 119
186838_1_En_14_Chapter_OnlinePDF.pdf 120
Receptivity of a supersonic boundary layer to shock-wave oscillations 120
1 Introduction 120
2 Numerical Method 121
3 Results 121
4 Conclusions 125
References 125
186838_1_En_15_Chapter_OnlinePDF.pdf 126
Roughness receptivity studies in a 3-D boundary layer – Flight tests and computations 126
1 Introduction 126
2 Cp Measurements 127
3 Critical DREs 128
4 Receptivity Measurements 129
5 Receptivity Results 130
References 131
186838_1_En_16_Chapter_OnlinePDF.pdf 132
DNS investigations of steady receptivity mechanisms on a swept cylinder 132
1 Geometry, main assumptions 132
2 Unexpected unsteady fluctuation 133
3 Steady perturbation 134
3.1 Considered shapes of the perturbation 135
3.2 Steady crossflow mode 135
3.3 Influence of the roughness element shape 136
References 137
186838_1_En_17_Chapter_OnlinePDF.pdf 138
Experimental Study of the Incipient Spot Breakdown Controlled by Riblets 138
1 Introduction 138
2 Experimental Setup and Measurement Procedure 139
3 Results and Discussion 140
4 Conclusions 142
References 142
186838_1_En_18_Chapter_OnlinePDF.pdf 144
Control of Stationary Cross-flow Modes Using Patterned Roughness at Mach 3.5 144
1 Experimental Approach 145
2 Results 146
2.1 Flow Visualization 146
2.2 Mean Velocity Measurements 147
3 Conclusions 148
References 149
186838_1_En_19_Chapter_OnlinePDF.pdf 150
Secondary optimal growth and subcritical transition in the plane Poiseuille flow 150
1 Introduction and background 150
2 Results and discussion 152
References 155
186838_1_En_20_Chapter_OnlinePDF.pdf 156
Disturbance evolution in rotating-disk boundary layers: competition between absolute instability and global stability 156
1 Introduction 156
2 Modelling of numerical simulation results 157
3 Simulation results for cases with mass transfer 158
4 Summary 161
References 161
186838_1_En_21_Chapter_OnlinePDF.pdf 162
Instabilities due a vortex at a density interface: gravitational and centrifugal effects 162
1 Introduction 162
2 Centrifugal effects 163
3 Gravitational effects 165
4 Conclusions and outlook 166
References 167
186838_1_En_22_Chapter_OnlinePDF.pdf 168
Wave Packets of Controlled Velocity Perturbations at Laminar Flow Separation 168
1 Introduction 168
2 Experimental set-up 169
3 Results and discussion 170
References 173
186838_1_En_23_Chapter_OnlinePDF.pdf 174
Linear Stability Analysis for Manipulated Boundary-Layer Flows using Plasma Actuators 174
1 Introduction 174
2 Linear Stability Analysis 175
3 Results 176
4 Discussion 179
References 179
186838_1_En_24_Chapter_OnlinePDF.pdf 180
Stripy patterns in low-Re turbulent plane Couette flow 180
1 Introduction 180
2 Results 181
2.1 Numerical method 181
2.2 Formation of stripes 182
References 185
186838_1_En_25_Chapter_OnlinePDF.pdf 186
Characterization of the three-dimensiona linstability in a lid-driven cavity by an adjoint based analysis 186
1 Introduction 186
2 Governing equations and solution method 187
3 Results 188
References 191
186838_1_En_26_Chapter_OnlinePDF.pdf 192
Bi-global crossplane stability analysis of high-speed boundary-layer flows with discrete roughness 192
1 Introduction 192
2 Bi-global secondary linear stability theory & numerics
3 Primary state 193
4 Results 194
5 Conclusions 197
References 197
186838_1_En_27_Chapter_OnlinePDF.pdf 198
Time-resolved PIV investigations on the laminar-turbulent transition over laminar separation bubbles 198
1 Introduction 198
2 Experimental setup and data evaluation 199
3 Results 199
4 Conclusion 202
References 202
186838_1_En_28_Chapter_OnlinePDF.pdf 204
Control of transient growth induced boundary layer transition using plasma actuators 204
1 Introduction 204
2 Experimental Details 205
3 Results 206
4 Conclusions and Outlook 208
References 209
186838_1_En_29_Chapter_OnlinePDF.pdf 210
Laminar Flow Control by Suction at Mach 2 210
1 Introduction 210
2 Experimental Set-Up 211
3 Experimental Results 211
4 Numerical Analyses 213
5 Conclusions 215
References 215
186838_1_En_30_Chapter_OnlinePDF.pdf 216
Decay of turbulent bursting in enclosed flows 216
1 Introduction 216
2 Methods 217
3 Results 217
4 Conclusion and outlook 220
References 221
186838_1_En_31_Chapter_OnlinePDF.pdf 222
Local and Global Stability of Airfoil Flows at Low Reynolds Number 222
1 Introduction 222
2 Behaviour with incidence 224
3 Influence of compressibility 225
4 Influence of Reynolds Number and Airfoil Geometry 225
5 Conclusion 226
References 227
186838_1_En_32_Chapter_OnlinePDF.pdf 228
Numerical simulation of riblet controlled oblique transition 228
1 Introduction 228
2 Numerical Method 229
3 Flow configuration and computational mesh 230
4 Results 230
References 231
186838_1_En_33_Chapter_OnlinePDF.pdf 234
Transition Movement in theWake of Protruding and Recessed Three-Dimensional Surface Irregularities 234
1 Introduction 234
2 Transition Measurements 235
3 Stability Calculations 236
4 Conclusions 237
References 238
186838_1_En_34_Chapter_OnlinePDF.pdf 240
Plasma Assisted Aerodynamics for Transition Delay 240
1 Introduction 240
2 Theoretical Background 241
2.1 Plasma model 241
3 Results 242
4 Conclusions and Future work 244
References 245
186838_1_En_35_Chapter_OnlinePDF.pdf 246
Experimental study on stability of the laminar and turbulent plane jets 246
1 Laminar plane jet with the abrupt mean velocity profile at the nozzle exit 246
2 A laminar and turbulent plane jet with a parabolic mean velocity profile at the nozzle exit 248
3 Plane jet approaching to the microjet 250
4 Conclusions 251
References 251
186838_1_En_36_Chapter_OnlinePDF.pdf 252
Evolution Of Traveling Crossflow Modes Over A Swept Flat Plate 252
1 Introduction 252
2 Experimental Setup 252
2.1 Turbulence generation 254
3 Results 254
3.1 Velocity and Disturbance Profiles 254
3.2 Spanwise Correlations 255
3.3 Disturbance Growth 256
4 Conclusions and Outlook 257
References 257
186838_1_En_37_Chapter_OnlinePDF.pdf 258
Computational Analysis for Roughness-Based Transition Control 258
1 Introduction 258
2 Methods 259
3 Results 259
4 Conclusions 263
References 263
186838_1_En_38_Chapter_OnlinePDF.pdf 264
Statistics of turbulent-to-laminar transition in plane Couette flow 264
1 Introduction 264
2 Model and Results 265
References 267
186838_1_En_39_Chapter_OnlinePDF.pdf 268
Spectra of Swirling Flow 268
1 Introduction 268
2 Linear asymptotical stability analysis 269
3 Optimal transient growth analysis 270
4 Map of spectra 271
5 Conclusion 273
References 273
186838_1_En_40_Chapter_OnlinePDF.pdf 274
Localized edge states for the transition to turbulence in shear flows 274
1 Introduction 274
2 Numerical methods and results 276
3 Conclusions 278
References 279
186838_1_En_41_Chapter_OnlinePDF.pdf 280
Active steady control of vortex shedding: an adjoint-based sensitivity approach 280
1 Introduction 280
2 Global stability of the cylinder flow 281
3 Adjoint-based sensitivity approach 282
4 Results 283
References 285
186838_1_En_42_Chapter_OnlinePDF.pdf 286
Feedback control of transient energy growth in subcritical plane Poiseuille flow 286
1 Introduction 287
2 Discretization 287
3 System properties 288
4 Control design 288
5 Results 289
6 Conclusions 291
References 291
186838_1_En_43_Chapter_OnlinePDF.pdf 292
Linear and non-linear disturbance evolution in a compressible boundary-layer with localized roughness 292
1 Introduction 292
2 Mathematical model and numerical method 293
3 Uncertainty quantification 294
4 Mean flow 294
5 Deterministic disturbance evolution 295
6 Stochastic disturbance evolution 296
7 Conclusion 297
References 297
186838_1_En_44_Chapter_OnlinePDF.pdf 298
Experimental Study of Boundary Layer Transition Subjected toWeak Free Stream Turbulence 298
1 Introducution 298
2 Experimental Set-up 299
3 Hot-wire Measurement Result and Flow Visualization 301
4 Conclution 303
References 303
186838_1_En_45_Chapter_OnlinePDF.pdf 304
Open-loop control of compressible afterbody flows using adjoint methods 304
1 Introduction 304
2 Theoretical framework 305
3 Results 307
4 Perspectives 308
References 309
186838_1_En_46_Chapter_OnlinePDF.pdf 310
Direct Numerical Simulation of a Swept-Wing Boundary Layer with an Array of Discrete Roughness Elements 310
1 Introduction 310
2 Flow Configuration and Numerical Method 311
3 Initial results and future work 313
References 315
186838_1_En_47_Chapter_OnlinePDF.pdf 316
Wave packet pseudomodes upstream of a swept cylinder 316
1 Introduction 316
2 Wave packet pseudomodes for the uniform stability problem 319
3 Conclusions 321
References 321
186838_1_En_48_Chapter_OnlinePDF.pdf 322
Bypass Transition prediction using a model based on transient growth theory 322
1 Introduction 322
2 Governing equations 323
3 Wall normal velocity fluctuation modelling 324
4 Results 324
5 Conclusion 326
References 327
186838_1_En_49_Chapter_OnlinePDF.pdf 328
Flow in a Slowly Divergent Pipe Section 328
1 Introduction 328
2 Experimental Setup 329
3 Results and Discussions 331
4 Conclusions 332
References 333
186838_1_En_50_Chapter_OnlinePDF.pdf 334
In-flight experiments on active TS-wave control on a 2D-laminar wing glove 334
1 Introduction 334
2 Experimental setup 335
3 Control algorithm 336
4 Results 337
5 Conclusions 339
References 339
186838_1_En_51_Chapter_OnlinePDF.pdf 340
Global nonlinear dynamics of thin aerofoil wakes 340
1 Introduction 340
2 Global nonlinear dynamics obtained by direct numerical simulations 341
3 Basic flow and local absolute frequencies 342
4 Discussion 344
References 345
186838_1_En_52_Chapter_OnlinePDF.pdf 346
Riccati-less optimal control of bluff-body wakes 346
1 Background 346
2 Riccati-less optimal control 348
3 Application 350
References 351
186838_1_En_53_Chapter_OnlinePDF.pdf 352
Asymptotic theory of the pre-transitional laminar streaks and comparison with experiments 352
1 Introduction 352
2 Mathematical formulation 353
3 Results 355
4 Conclusions and Outlook 356
References 357
186838_1_En_54_Chapter_OnlinePDF.pdf 358
Roughness-induced transition of compressible laminar boundary layers 358
1 Introduction 358
2 Method 359
3 Flow structure 360
4 Critical threshold 361
5 Conclusion 362
References 363
186838_1_En_55_Chapter_OnlinePDF.pdf 364
On receptivity and modal linear instability of laminar separation bubbles at all speeds 364
1 Introduction and Motivation 364
2 Theory and Numerical Methods 365
3 Results 366
3.1 Incompressible flow 366
3.1.1 Receptivity and sensitivity of LSB flow 366
3.1.2 U-separation and Stall Cells 367
3.2 Compressible flow 368
3.2.1 Subsonic flow: the effect of compressibility 368
3.2.2 Supersonic regime: SBLI and supersonic finite-angle wedge flows 368
References 369
186838_1_En_56_Chapter_OnlinePDF.pdf 370
Hypersonic instability waves measured on a circular cone at M=12 using fast-response surface heat-flux and pressure gauges 370
1 Introduction 370
2 Experimental Setup 370
3 Experimental Results 372
References 375
186838_1_En_57_Chapter_OnlinePDF.pdf 376
Interaction of noise disturbances and streamwise streaks 376
1 Introduction and Numerical Method 376
2 Numerical Method 377
3 Results 378
4 Conclusions 381
References 381
186838_1_En_58_Chapter_OnlinePDF.pdf 382
Experimental study on the use of the wake instability as a passive control in coaxial jet flows 382
1 Introduction 382
2 Experimental arrangement 383
3 Results 384
4 Conclusions 387
References 387
186838_1_En_59_Chapter_OnlinePDF.pdf 388
Numerical and Experimental Investigations of Relaminarizing Plane Channel Flow 388
1 Introduction 388
2 Numerical Method and Experimental Setup 389
2.1 Numerical Method 389
2.2 Experimental Facility and Measurement Technique 390
3 Results 390
4 Conclusion 393
References 393
186838_1_En_60_Chapter_OnlinePDF.pdf 394
Linear control of 3D disturbances on a flat-plate 394
1 Input-output configuration 394
2 Model reduction 396
3 Controller design 398
References 399
186838_1_En_61_Chapter_OnlinePDF.pdf 400
Experimental study of stability of supersonic boundary layer on swept wing 400
1 Introduction 400
2 Experimental equipment 401
3 Stability 402
4 Conclusions 404
References 405
186838_1_En_62_Chapter_OnlinePDF.pdf 406
Comparison of Direct Numerical Simulation with the Theory of Receptivity in a Supersonic Boundary Layer 406
1 Introduction 406
2 Problem formulation 407
3 Analysis and results 408
4 Conclusions 410
References 411
186838_1_En_63_Chapter_OnlinePDF.pdf 412
Instability of high Mach number flows in the presence of high-temperature gas effects 412
1 Introduction 412
2 Numerical Method 413
2.1 Results 414
2.1.1 Instability development in the M=20 flat plate boundary layer 414
2.2 Flow around the cuboid in the HyBoLT configuration 415
2.3 Conclusions 416
References 417
186838_1_En_64_Chapter_OnlinePDF.pdf 418
Spatially localised growth within global instabilities of flexible channel flows 418
1 Introduction 418
2 The model 419
3 Methods 421
4 Results 422
5 Discussion 422
References 423
186838_1_En_65_Chapter_OnlinePDF.pdf 424
Global stability of a plane liquid jet surrounded by gas 424
1 Introduction 424
2 Flow modelling, numerical implementation and verification 426
3 Results and discussion 428
4 Conclusions and outlook 429
References 429
186838_1_En_66_Chapter_OnlinePDF.pdf 430
Instabilities of flow in a corrugated pipe 430
1 Introduction 430
2 A model of corrugated pipe and stability analysis 431
3 Conclusions 435
References 435
186838_1_En_67_Chapter_OnlinePDF.pdf 436
The Late Nonlinear Stage of Oblique Breakdown to Turbulence in a Supersonic Boundary Layer 436
1 Introduction 436
2 Computational Setup 437
3 Initiating the Oblique Breakdown Mechanism 438
4 The Late Nonlinear Stage of Breakdown 439
5 Reaching Fully Developed Turbulence 440
6 Conclusions 441
References 441
186838_1_En_68_Chapter_OnlinePDF.pdf 442
Turbulence stripe in transitional channel flow with/without system rotation 442
1 Introduction 442
2 Numerical and experimental descriptions 443
3 Results 444
3.1 DNS on PPF and PCF 444
3.2 Flow visualization on PPF and RPCF 445
4 Conclusions 447
References 447
186838_1_En_69_Chapter_OnlinePDF.pdf 448
Direct Numerical Simulation and Theoretical Analysis of Perturbations in Hypersonic Boundary Layers 448
1 Introduction 448
2 Outline of the method 449
3 Numerical Approach 450
4 Results 450
4.1 Flat plate 450
4.2 Wedge 453
References 453
186838_1_En_70_Chapter_OnlinePDF.pdf 454
Flow Transition in Free Liquid Film Induced by Thermocapillary Effect 454
1 Introduction 454
2 Target Geometry 455
3 Numerical Simulation 456
4 Experiment 456
5 Results & Discussion
6 Concluding Remarks 459
References 459
186838_1_En_71_Chapter_OnlinePDF.pdf 460
Boundary layer transition by interaction of streaks and Tollmien–Schlichting waves 460
1 Introduction 461
2 Interaction of streaks and Tollmien–Schlichting waves 462
Continuous-discrete mode interactions 462
The influence of free-stream turbulence 464
References 465
186838_1_En_72_Chapter_OnlinePDF.pdf 466
Numerical Investigation of Subharmonic Resonance Triads in a Mach 3 Boundary Layer 466
1 Introduction 466
2 Computational Setup 467
3 Subharmonic Resonance Triad 468
4 DNS of Oblique-Subharmonic Resonance Triad 469
5 DNS of the Interaction of Oblique-Subharmonic Resonance with Oblique Breakdown 470
6 Conclusions 471
References 471
186838_1_En_73_Chapter_OnlinePDF.pdf 473
Transient Growth on the Homogenous Mixing Layer 473
1 Introduction 473
2 Hyperbolic Tangent Velocity Profile 474
3 Developing KH billow 476
References 476
186838_1_En_74_Chapter_OnlinePDF.pdf 477
Closed-loop control of cavity flow using a reduced-order model based on balanced truncation 477
1 Introduction 477
2 Configuration, modeling and model reduction 478
3 LQG control 478
4 Comparison with reduced model based on POD and global modes 480
5 Conclusions and Outlook 480
References 480
186838_1_En_75_Chapter_OnlinePDF.pdf 481
On the asymptotic solution of the flow around a circular cylinder 481
1 Introduction 481
2 Numerical Simulations 482
3 Experiments and DPIV Mesurements 482
4 Results: harmonic fields and amplitudes 483
5 Acknowledgements 484
References 484
186838_1_En_76_Chapter_OnlinePDF.pdf 485
Investigations of Suction in a Transitional Flat-Plate Boundary Layer 485
1 Introduction 485
2 Experimental setup 486
3 Results 487
4 Conclusion 488
References 488
186838_1_En_77_Chapter_OnlinePDF.pdf 489
Global three-dimensional optimal perturbations in a Blasius boundary layer 489
1 Introduction 489
2 Problem formulation 490
3 Results and discussion 490
References 492
186838_1_En_78_Chapter_OnlinePDF.pdf 493
Quantifying sub-optimal transient growth using biorthogonal decomposition 493
1 Motivation 493
2 Method 494
3 Results 495
References 496
186838_1_En_79_Chapter_OnlinePDF.pdf 497
Model reduction using Balanced Proper Orthogonal Decomposition with frequential snapshots 497
1 Introduction 497
2 Flow configuration 498
3 Model reduction 498
4 Input-output response 499
5 Conclusions and Outlook 500
References 500
186838_1_En_80_Chapter_OnlinePDF.pdf 501
Control of a trapped vortex in a thick airfoil by steady/unsteady mass flow suction 501
1 Introduction 501
2 Experimental Setup and Measurements Instrumentation 501
3 Experimental Test Campaign 502
3.1 No-Suction and Steady Suction 502
3.2 Unsteady Suction 503
4 Results 503
5 Conclusions 504
References 504
186838_1_En_81_Chapter_OnlinePDF.pdf 505
Receptivity of compressible boundary layer to kinetic fluctuations 505
1 Introduction 505
2 Analysis and results 506
3 Conclusions 508
References 508
186838_1_En_82_Chapter_OnlinePDF.pdf 509
Effect of transport modeling on hypersonic cooled wall boundary layer stability 509
1 Introduction 509
2 Methodology 510
3 Results 511
4 Conclusion 512
References 512
186838_1_En_83_Chapter_OnlinePDF.pdf 513
Modeling Supersonic and Hypersonic Flow Transition over Three-Dimensional Bodies 513
1 Introduction 513
2 Model formulation 514
3 Results and discussion 514
4 Conclusion 516
References 516
186838_1_En_84_Chapter_OnlinePDF.pdf 517
Amplitude threshold in the wake transition of an oscillating circular cylinder 517
1 Introduction 517
2 Results 518
3 Conclusions 519
4 Acknowledgements 520
References 520
186838_1_En_85_Chapter_OnlinePDF.pdf 521
Certain Aspect of Instability of Flow in a Channel with Expansion/Contraction 521
1 Introduction 521
2 Numerical procedure 522
3 Results and Discussion 523
References 523
186838_1_En_86_Chapter_OnlinePDF.pdf 525
Some properties of boundary layer under the joint effect of external flow turbulence and surface roughness 525
1 Introduction 525
2 Experiment and results 526
3 Conclusions 527
References 528
186838_1_En_87_Chapter_OnlinePDF.pdf 529
Wave forerunners of localized structures at the boundary layer 529
1 Introduction 529
2 Experimental set-up 529
3 Results 530
4 Conclusions 532
References 532
186838_1_En_88_Chapter_OnlinePDF.pdf 533
Experiments on the wave train excitation and wave interaction in spanwise modulated supersonic boundary layer 533
1 Introduction 533
2 Experiments set-up 534
3 Results 534
3.1 Initial Amplitudes of Wave Trains 535
3.2 Nonlinear Wave Train Development 535
4 Conclusions 536
References 536
186838_1_En_89_Chapter_OnlinePDF.pdf 537
Laminar-Turbulent Transition and Boundary Layer Separation on wavy surface wing 537
1 Introduction 537
2 Experimental Apparatus 538
3 Results 538
4 Conclusion 539
References 539
186838_1_En_90_Chapter_OnlinePDF.pdf 540
Investigation of Thermal Nonequilibrium on Hypersonic Boundary-Layer Transition by DNS 540
1 Gas Models 540
2 Results 541
3 Conclusions 543
References 543
186838_1_En_91_Chapter_OnlinePDF.pdf 544
Global sustained perturbations in a backward-facing step flow 544
1 Introduction 544
2 Global sustained perturbations 545
3 Results 547
References 547
186838_1_En_92_Chapter_OnlinePDF.pdf 548
Large Reynolds number streak description using RNS 548
1 RNS streak formulation 548
2 Results and Conclusions 550
3 Acknowledgments 551
References 551
186838_1_En_93_Chapter_OnlinePDF.pdf 552
Optimal disturbances with iterative methods 552
1 Optimal disturbances with iterative methods 552
2 Results 553
3 Conclusions 555
References 555
186838_1_En_94_Chapter_OnlinePDF.pdf 556
Connection between full-lifetime and breakdown of puffs in transitional pipe flows 556
1 Introduction 556
2 Experimental test rig 557
3 Measurement of a full-lifetime of puffs and a rate of splitting puffs’ occurrence 557
4 Conclusions and final remarks 558
References 559
186838_1_En_95_Chapter_OnlinePDF.pdf 560
Effect of oblique waves on jet turbulence 560
1 Introduction 560
2 Motivation for experiments 561
3 Results and Discussion 562
References 563
186838_1_En_96_Chapter_OnlinePDF.pdf 564
The effect of a single three-dimensional roughness element on the boundary layer transition 564
1 Introduction 564
2 Experimental Set-up and Results 565
3 Final remarks 565
References 567
186838_1_En_97_Chapter_OnlinePDF.pdf 568
Experimental study of resonant interactions of modulated waves in a non self-similar boundary layer 568
1 Introduction 568
2 Results 569
3 Conclusions 570
References 571
186838_1_En_98_Chapter_OnlinePDF.pdf 572
High Reynolds Number Transition Experiments in ETW (TELFONA project) 572
1 Introduction 572
2 Model Design and measurement systems 573
3 Analysis and stabilty calculations 574
4 Conclusion 575
186838_1_En_99_Chapter_OnlinePDF.pdf 576
Entropy generation rate in turbulent spots in a boundary layer subject to freestream turbulence 576
1 Introduction 576
2 Results and Discussion 577
2.1 Spot Evolution 577
2.2 Entropy generation 578
3 Conclusions 578
References 579
186838_1_En_100_Chapter_OnlinePDF.pdf 580
The Effect of a Particle travelling through a Laminar Boundary Layer on Transition 580
1 Background 580
2 ExperimentalWork 581
3 NumericalWork 582
4 Concluding Remarks 583
References 583
186838_1_En_101_Chapter_OnlinePDF.pdf 584
Flow past a plate with elliptic leading edge: layer response to free-stream vorticity 584
1 Introduction 584
2 Flow Model and Numerical Approach 585
3 Results 585
References 587
186838_1_En_102_Chapter_OnlinePDF.pdf 588
Fluctuation Measurements in the Turbulent Boundary Layer of a Supersonic Flow 588
1 Introduction 588
2 Experimental Facility 589
3 Measurement Devices and Data Evaluation 589
4 Results and Discussion 590
5 Conclusions and Outlook 591
References 591
186838_1_En_103_Chapter_OnlinePDF.pdf 592
Experimental characterization of the transition region in a rotating-disk boundary layer 592
1 Introduction 592
2 Experimental setup 593
3 Mean-velocity profiles 593
4 Spectral analysis 593
5 Conclusions and outlook 595
References 595
186838_1_En_104_Chapter_OnlinePDF.pdf 596
Nonlinear Interaction BetweenWavepackets in Plane Poiseuille Flow 596
1 Introduction 596
2 Equations, Numerical Methods and Initial Condition 597
3 Results 597
4 Final Remarks 598
References 599
186838_1_En_105_Chapter_OnlinePDF.pdf 600
Effects of Passive PorousWalls on Hypersonic Boundary Layers 600
1 Introduction 600
2 Linear Stability Problem 601
3 Results 602
4 FutureWork 602
References 603
186838_1_En_106_Chapter_OnlinePDF.pdf 604
Global Instabilities inWall Jets 604
1 Introduction 604
2 Formulation and Numerical Method 605
3 Results 605
4 Conclusions 607
References 607
186838_1_En_107_Chapter_OnlinePDF.pdf 608
Spatial Optimal Disturbances in Three-Dimensional Boundary Layers 608
1 Introduction 608
2 Methodology 609
3 Results 610
References 611
186838_1_En_108_Chapter_OnlinePDF.pdf 612
Influence of turbulence scale and shape of leading edge on laminar-turbulent transition induced by free-stream turbulence 612
1 Introduction 612
2 Linear receptivity theory to FST 613
3 Experimental results 614
References 615
186838_1_En_109_Chapter_OnlinePDF.pdf 616
Bifurcation characteristics of the channel flow on a rotating system undergoing transition under the influence of the Coriolis force 616
1 Introduction and scope of the present work 616
2 The governing equations 617
3 Outline of the method 617
4 Conclusions and Outlook 619
References 619
186838_1_En_110_Chapter_OnlinePDF.pdf 620
Linear Stability Investigations of Flow Over Yawed Anisotropic CompliantWalls 620
1 Introduction 620
2 Theoretical Model of the Yawed AnisotropicWall 620
3 Numerical Method and Code Validation 621
4 Results 622
5 Conclusions 622
References 623
186838_1_En_BookBackmatter_OnlinePDF.pdf 624
Author Index 624
Part I Invited Presentations 24
Part II Oral Presentations 89
Part III Poster Presentations 472

Erscheint lt. Verlag 11.3.2010
Reihe/Serie IUTAM Bookseries
IUTAM Bookseries
Zusatzinfo XXIV, 608 p.
Verlagsort Dordrecht
Sprache englisch
Themenwelt Naturwissenschaften Physik / Astronomie Strömungsmechanik
Technik Maschinenbau
Schlagworte experimental techniques • flow control • fluid- and aerodynamics • Hydrodynamic Stability • IUTAM • numerical simulations of fluid flow • Riblet • Transition to Turbulence
ISBN-10 90-481-3723-3 / 9048137233
ISBN-13 978-90-481-3723-7 / 9789048137237
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