E-Book, Englisch, 822 Seiten
Choi Computational Fluid Dynamics 2008
1. Auflage 2009
ISBN: 978-3-642-01273-0
Verlag: Springer
Format: PDF
Kopierschutz: Adobe DRM (»Systemvoraussetzungen)
E-Book, Englisch, 822 Seiten
ISBN: 978-3-642-01273-0
Verlag: Springer
Format: PDF
Kopierschutz: Adobe DRM (»Systemvoraussetzungen)
Autoren/Hrsg.
Weitere Infos & Material
1;Preface;5
2;Contents;6
3;Part 1 Plenary Lectures;19
3.1;Lattice Boltzmann Methods for Viscous Fluid Flows and Two-Phase Fluid Flows;20
3.1.1;Introduction;20
3.1.2;Lattice Boltzmann Method;21
3.1.2.1;Lattice Gas Model and Evolution Equation;21
3.1.2.2;Lattice Boltzmann Method for Temperature Field;22
3.1.2.3;Boundary Condition;23
3.1.2.4;Governing Equations for Macroscopic Variables;23
3.1.2.5;Numerical Examples;24
3.1.3;Lattice Boltzmann Method for Two-Phase Fluids;25
3.1.3.1;Formulation;25
3.1.3.2;Algorithm of Computation;28
3.1.3.3;Governing Equations for Macroscopic Variables;28
3.1.3.4;Numerical Examples;29
3.1.4;Concluding Remarks;31
3.1.5;References;33
3.2;Coping with Uncertainty in Turbulent Flow Simulations;35
3.2.1;Introduction;35
3.2.2;Inertial Range Consistent Subgrid/Turbulence Models;36
3.2.3;The Concept of Robust Modelling;38
3.2.4;Copping with Uncertainties: Response Surface;40
3.2.5;Concluding Remarks;44
3.2.6;References;45
3.3;Adaptive Finite Element Discretization of Flow Problems for Goal-Oriented Model Reduction;47
3.3.1;Introduction;47
3.3.2;Goal-Oriented Adaptivity: Concept and Examples;48
3.3.2.1;Example 1. Drag Computation in 2-d Viscous Flow;48
3.3.2.2;Example 2. Drag Computation in 3-d Viscous Flow ([BR06]);50
3.3.2.3;Example 3. Inviscid 2-d Euler Equations ([Har02]);51
3.3.2.4;Example 4. A 2-d Heat-Driven Cavity Benchmark ([BR00]);52
3.3.3;The Theoretical Framework;53
3.3.3.1;Application in Flow Simulation;54
3.3.3.2;Practical Aspects;55
3.3.4;Applications;56
3.3.4.1;Drag Minimization by Boundary Control ([Bec01]);56
3.3.4.2;Fluid-Structure Interaction ([DR06]), [Dun07], [BDR08]);57
3.3.5;Summary and Outlook;59
3.3.6;References;60
4;Part 2 Keynote Lectures;62
4.1;Progress in Computational Magneto-Fluid-Dynamics for Flow Control;63
4.1.1;Introduction;63
4.1.2;Governing Equations;65
4.1.3;Model of Weakly Ionized Gas;66
4.1.4;Solving Scheme;67
4.1.5;Results of Numerical Simulation;69
4.1.6;Summary;73
4.1.7;References;73
5;Part 3 Aeroacoustics 1;75
5.1;Computation of Noise Radiated from a Turbulent Flow over a Cavity with Discontinuous Galerkin Method;76
5.1.1;Introduction;76
5.1.2;Numerical Formulations;77
5.1.3;Results and Discussions;78
5.1.4;Conclusions;80
5.1.5;References;81
5.2;Far–Field Noise Minimization Using an Adjoint Approach;82
5.2.1;Introduction;82
5.2.2;Noise Prediction Validation;82
5.2.3;Results;83
5.2.4;Conclusions;88
5.2.5;References;88
5.3;Stabilized High-Order Discontinuous Galerkin Methods for Aeroacoustic Investigations;89
5.3.1;Introduction;89
5.3.2;Stabilization;89
5.3.3;Stabilized Extrapolation Boundary Conditions;91
5.3.4;Numerical Tests;92
5.3.4.1;Flow Around a Cylinder at Re=100;92
5.3.4.2;Tone Hole Investigations;93
5.3.5;Conclusion;94
5.3.6;References;94
6;Part 4 Aeroacoustics 2;95
6.1;Direct Simulation for Acoustic Near Fields Using the Compressible Navier-Stokes Equation;96
6.1.1;Introduction;96
6.1.1.1;Prediction of Acoustic Resonance Phenomena;96
6.1.1.2;”The Theory of The Fluteh by M.S.Howe;97
6.1.1.3;Computational Problems for the Compressible Navier Stokes equation(C.N.S.E);97
6.1.1.4;Numerical Method;97
6.1.1.5;Transition to Turbulence;98
6.1.2;Bench Mark Computation;98
6.1.2.1;Bench Mark 1 :Edge-Tone;98
6.1.2.2;Bench Mark 2 :Recorder;99
6.1.3;Conclusion;101
6.1.4;References;101
6.2;Aeroacoustic Simulation in Automobile Muffler by Using the Exact Compressible Navier-Stokes Equation;103
6.2.1;Introduction;103
6.2.2;Objectives;104
6.2.3;Governing Equations;104
6.2.4;Numerical Method;104
6.2.5;Bench Mark Computation;105
6.2.5.1;Bench Mark 1: One Point Oscillator on a Cavity;105
6.2.5.2;Bench Mark 2: Flow Noise by Two Jets in a Round Chamber;106
6.2.6;Simulation of Automobile Muffler Model;106
6.2.6.1;Case1: Artificial(forcing) Oscillation at the Inlet;106
6.2.6.2;Case2: No Artificial Oscillation at the Inlet;107
6.2.7;Conclusion;108
6.2.8;References;108
7;Part 5 Aeroacoustics/Elasticity;109
7.1;Towards Understanding the Physics of Supersonic Jet Screech;110
7.1.1;Numerical Evidence;111
7.1.2;Theoretical Evidence;114
7.1.3;Experimental Evidence;115
7.1.4;Conclusion;115
7.1.5;References;115
7.2;Calculation of Wing Flutter Using Euler Equations with Approximate Boundary Conditions;116
7.2.1;Introduction;116
7.2.2;Numerical Methods;117
7.2.2.1;Governing Equations;117
7.2.2.2;Approximate Boundary Conditions;117
7.2.2.3;Structural Equation of Motion;118
7.2.3;Results and Discussion;118
7.2.3.1;ONERA M6Wing;118
7.2.3.2;LANN Wing;118
7.2.3.3;AGARD 445.6Wing;120
7.2.4;Conclusion;120
7.2.5;References;121
7.3;Direct Computation of Infrasound Propagation in Inhomogeneous Atmosphere Using a Low-Dispersion and Low-Dissipation Algorithm;122
7.3.1;Introduction;122
7.3.2;Case of the $Misty Picture$ experiment;123
7.3.2.1;Atmosphere Model;123
7.3.2.2;Governing Equations and Numerical Algorithm;124
7.3.3;Modelling of Atmospheric Sound Absorption in Time-Dependent Simulations;126
7.3.4;Concluding Remarks;126
7.3.5;References;127
8;Part 6 Algorithm 1;128
8.1;Symmetry Preserving Discretization of the Compressible Euler Equations;129
8.1.1;Introduction;129
8.1.2;Euler Equations;131
8.1.3;Discrete Invariant Method;132
8.1.4;Numerical Results;133
8.1.5;Conclusion;134
8.1.6;References;134
8.2;A Numerical Diffusion Flux Based on the Diffusive Riemannproblem;135
8.2.1;Introduction;135
8.2.2;The Generalized Diffusive Riemannproblem;136
8.2.3;The Use in High Order DG and FV schemes;138
8.2.4;Example: Compressible Navier-Stokes Equations;139
8.2.5;References;140
9;Part 7 Algorithm 2;141
9.1;Enhancement of the Computational Efficiency of UFP via a MWM;142
9.1.1;Introduction;142
9.1.2;Implementation of the Modified Wavelet Method;143
9.1.3;Numerical Test and Discussion;144
9.1.4;Conclusion;147
9.1.5;References;147
9.2;A High-Order Accurate Implicit Operator Scheme for Solving Steady Incompressible Viscous Flows Using Artificial Compressibility Method;148
9.2.1;References;152
9.3;Development of a Coupled and Unified Solution Method for Fluid-Structure Interactions;153
9.3.1;Introduction;153
9.3.2;Technical Approach;153
9.3.3;Results;156
9.3.4;References;158
10;Part 8 Algorithm 3;159
10.1;Development of AUSM-Type Solver for Analysis of Ideal Magnetohydrodynamic Flows;160
10.1.1;Introduction;160
10.1.2;Governing Equations;162
10.1.2.1;Ideal MHD Equations;162
10.1.2.2;Modifying the Ideal MHD Equations (Cleaning Divergence Errors);162
10.1.3;Numerical Method;163
10.1.3.1;AUSMPW+/M-AUSMPW+ Scheme of Ideal MHD Equations;163
10.1.3.2;A High Order Interpolation Scheme: OMLP;164
10.1.4;Numerical Results;164
10.1.4.1;Brio and Wu’s Shock Tube Test;164
10.1.4.2;2-D Cloud and Shock Interactions;166
10.1.5;Conclusions;170
10.1.6;References;171
10.2;An Implicit Parallel Fully Compressible Roe Based Solver for Subsonic and Supersonic Reacting Flows;172
10.2.1;Introduction;172
10.2.2;Theoretical Formulation and Numerical Treatment;172
10.2.2.1;Governing Equations;172
10.2.2.2;Numerical Modeling;173
10.2.2.3;Turbulence Modeling;173
10.2.2.4;Combustion Modeling;173
10.2.3;Coupling the EDM Model with the SA Model;173
10.2.4;Test Cases;175
10.2.4.1;Moreau’s Combustor;175
10.2.4.2;Kent’s and Bilger’s Combustor;175
10.2.4.3;Supersonic Flow over a Flat Plate with Injection Slot;175
10.2.5;Conclusion;176
10.2.6;References;177
11;Part 9 Bio-fluid Mechanics 1;178
11.1;Rheology of Blood Flow in a Branched Arterial System with Three-Dimension Model;179
11.1.1;Introduction;179
11.1.2;Materials and Methods;180
11.1.2.1;Power Law for Non-Newtonian Viscosity;180
11.1.2.2;Carreau Model;180
11.1.2.3;Casson Model;180
11.1.2.4;T-Junction Model;181
11.1.3;Results and Discussions;181
11.1.4;Conclusion;183
11.1.5;References;183
11.2;The Effect of Curvature and Torsion on Steady Flow in a Loosely Coiled Pipe;185
11.2.1;Introduction;185
11.2.2;Numerical Models and Methodology;186
11.2.3;Results;186
11.2.4;Conclusions;189
11.2.5;References;190
12;Part 10 Bio-fluid Mechanics 2;191
12.1;Analysis of the Unsteady Flow and Forces in an AAA Endovascular Stent;192
12.1.1;Introduction;192
12.1.2;Methods of Approach;193
12.1.3;Discussion;194
12.1.4;References;197
13;Part 11 Complex Flow 1;198
13.1;Computation of Low Reynolds Number Aerodynamic Characteristics of a Flapping Wing in Free Flight;199
13.1.1;Introduction;199
13.1.2;Computational Model;199
13.1.3;Results and Discussions;200
13.1.3.1;Effect of Outer Boundary Locations on Computed Aerodynamic Characteristics;200
13.1.4;Conclusion;204
13.1.5;References;204
13.2;Application of Window Embedment Grid Technique;205
13.2.1;Introduction;205
13.2.2;Introduction to Window Embedment Grid;206
13.2.3;Numerical Methods;207
13.2.3.1;Spatial Schemes;207
13.2.3.2;Turbulence Models;208
13.2.3.3;Time Advancing Schemes;208
13.2.4;Numerical Experiments;208
13.2.4.1;DLR-F4 Wing-Body Configuration;208
13.2.4.2;Application for Transporter Simulation;209
13.2.5;Conclusions;210
13.2.6;References;210
13.3;Improved Component Buildup Method for Fast Prediction of the Aerodynamic Performances of a Vertical Takeoff and Landing Micro Air Vehicle;211
13.3.1;Background;211
13.3.2;The Proposed Method;212
13.3.3;Validation;213
13.3.4;Conclusions;216
13.3.5;References;216
14;Part 12 Complex Flow 2;217
14.1;Numerical Investigation of the Tip Leakage Flow in a Multistage High Pressure Compressor;218
14.1.1;Introduction;218
14.1.2;Methodology;219
14.1.2.1;Compressor Test Case;219
14.1.2.2;Numerical Method;220
14.1.2.3;Numerical Model Validation and Results;223
14.1.3;Flow Analysis;224
14.1.3.1;Investigation of the Small Tip Clearance Case;224
14.1.3.2;Investigation of the Large Tip Clearance Case;227
14.1.4;Conclusion;228
14.1.5;References;229
15;Part 13 Complex Flows 3;231
15.1;Computational and Experimental Studies of Fluid Flow and Heat Transfer in a Calandria Based Reactor;232
15.1.1;Introduction;232
15.1.2;Calendria Model and Mesh Generation;233
15.1.3;Governing Equations and Boundary Condition;233
15.1.4;Results of Experimental and Computational Analysis;234
15.1.4.1;Computational Results;234
15.1.4.2;Experimental Results;236
15.1.5;Conclusions;237
15.1.6;References;237
16;Part 14 Complex Flows 4;238
16.1;Propulsion by an Oscillating Thin Airfoil at Low Reynolds Number;239
16.1.1;Introduction;239
16.1.2;Computational Method;240
16.1.3;TestCase;240
16.1.4;Heaving Motion;241
16.1.5;Pitching Motion;242
16.1.6;Summary and Further Research;244
16.1.7;References;244
16.2;Residual Currents around Plural Asymmetrical Structures in Oscillatory Flow Fields;245
16.2.1;Introduction;245
16.2.2;Computational Method;246
16.2.3;The Effects of the Asymmetrical Structures;246
16.2.4;The Effects of the Space between the Structures;248
16.2.5;Conclusions;250
16.2.6;References;250
17;Part 15 Compressible Flow 1;251
17.1;Stability of the MUSCL Method on General Unstructured Grids for Applications to Compressible Fluid Flow;252
17.1.1;Introduction;252
17.1.2;Slope Reconstruction on General Unstructured Meshes;253
17.1.3;Stability Analysis of the {\sc Muscl} Scheme;254
17.1.4;Numerical Computation of Spectra of Muscl Operators;255
17.1.5;Applications to Compressible Gas Dynamics;256
17.1.6;References;257
17.2;Time-Accurate Computational Analysis of the Flame Trench;258
17.2.1;Introduction;258
17.2.2;Computational Model;259
17.2.3;OVERFLOWSolver;260
17.2.4;Two-SRB Results;260
17.2.5;Single SRB Results;261
17.2.6;Summary;263
17.2.7;References;263
17.3;Very High Order Residual Distribution Schemes for Steady Flow Problems;265
17.3.1;Description of the Scheme;265
17.3.1.1;Numerical Approximation, Degrees of Freedom;266
17.3.1.2;Residual Computation and Distribution;266
17.3.2;Numerical Simulations for the Non Viscous Problem;267
17.3.3;Navier-Stokes Problems;268
17.3.4;Conclusion;270
17.3.5;References;270
18;Part 16 Compressible Flow 2;271
18.1;Shocks in Direct Numerical Simulation of the 3-D Spatially Developing Plane Mixing Layer;272
18.1.1;Introduction;272
18.1.2;Basic Equations, Initial Conditions and Numerical Methods;272
18.1.3;Computational Results;273
18.1.3.1;Visualization of Shocks;273
18.1.3.2;Categorization of Shocks;275
18.1.4;Conclusion;277
18.1.5;References;277
18.2;Calculation of Aerodynamic Performance of Propellers at Low Reynolds Number Based on Reynolds-Averaged Navier-Stokes Equations Simulation;278
18.2.1;Introduction;278
18.2.2;Governing Equations;278
18.2.3;Numerical Method;279
18.2.4;Grid System and Boundary Conditions;280
18.2.5;Numerical Results and Analysis;281
18.2.6;Concluding Remarks;283
18.2.7;References;283
18.3;Mathematical Modeling of Supersonic Turbulent Flows in a Channel of Variable Cross-Section with Mass Supply;284
18.3.1;Introduction;284
18.3.2;Problem Statement and Flow Condition;284
18.3.3;Method of Computation;285
18.3.4;Test Computations;286
18.3.5;Numerical Results;287
18.3.6;Conclusions and Future Work;289
18.3.7;References;289
18.4;Efficient Numerical Simulation of Dense Gas Flows Past Airfoils and Wings;290
18.4.1;Introduction;290
18.4.2;Governing Equations and Thermodynamical Model;290
18.4.3;Space and Time Discretization;292
18.4.4;Numerical Results;293
18.4.5;References;295
18.5;A Dual-Time Implicit Upwind Scheme for Computing Three-Dimensional UnsteadyCompressible Flows Using Unstructured Moving Grids;296
18.5.1;Introduction;296
18.5.2;Mesh Movement Strategy;296
18.5.3;Solution Algorithm;297
18.5.4;Results and Discussion;299
18.5.5;References;301
19;Part 17 Error Estimation and Control;302
19.1;Problems Associated with Grid Convergence of Functionals;303
19.1.1;Introduction;303
19.1.2;Order-Of-Convergence of Functionals;306
19.1.3;The Problem with Quadrature;306
19.1.4;How to Eliminate the Quadrature Error;306
19.1.5;Higher-Order Algorithmic Error Model;307
19.1.6;Conclusions and Recommendations;308
19.1.7;References;308
19.2;Accuracy Analysis Based on a Posteriori Error Estimates of SemiGLS Stabilization of FEM for Solving Navier-Stokes Equations;309
19.2.1;Introduction;309
19.2.2;Mixed FEM Formulation;309
19.2.3;SemiGLS Stabilized Formulation;310
19.2.4;A Posteriori Error Estimates;310
19.2.5;Numerical Results and Accuracy Analysis;311
19.2.5.1;Steady Flow in Lid Driven Cavity;311
19.2.5.2;Steady Flow in Channel with Sudden Extension of Diameter;312
19.2.6;Conclusion;313
19.2.7;References;314
19.3;Residual Adaptive Computations of Complex Turbulent Flows;315
19.3.1;Introduction;315
19.3.2;Residual Error Estimation;316
19.3.3;Adaptation Algorithm;316
19.3.4;Grid and Solution Methodology;317
19.3.5;Numerical Simulations;318
19.3.6;Conclusion;320
19.3.7;References;320
20;Part 18 Flow Control/Instability;321
20.1;Active Control of Transitional Channel Flows with Pulsed and Synthetic Jets Using Vortex Methods;322
20.1.1;Context and Aim of the Study;322
20.1.2;Numerical Scheme;323
20.1.3;Control Strategies;323
20.1.4;Numerical Results;324
20.1.4.1;First Control Type;324
20.1.4.2;Second ontrol ype;326
20.1.5;Conclusion;327
20.1.6;References;327
20.2;Numerical Analysis of Control Problems for Stationary Models of Hydrodynamics and Heat Transfer;328
20.2.1;Statement of the Direct Boundary Problem;328
20.2.2;Control Problems;330
20.2.3;Numerical Analysis;331
20.2.4;References;333
20.3;Frictional and Radiation Dampings on Shear Instability;334
20.3.1;Introduction;334
20.3.2;Formulation;335
20.3.3;Stability;337
20.3.4;Conclusion;339
20.3.5;References;339
20.4;FSI Analysis of HAR Wing at Low Speed Flight Condition;340
20.4.1;Introduction;340
20.4.2;VMT Method;341
20.4.3;Transfer of Structure’s Displacement;342
20.4.4;Fluid-Structure Interaction Analysis;342
20.4.5;Wing Model;342
20.4.6;Results;343
20.4.6.1;Static Deflection under Gravity Loading;343
20.4.6.2;Static Aeroelastic Deflections of the Wing;343
20.4.7;References;345
21;Part 19 Flow in Porous Media;346
21.1;3-D Numerical Simulation of Main Sieve Diaphragm with Three Types Passageway Design in a Gas Mask Canister;347
21.1.1;Introduction;347
21.1.2;Problem;349
21.1.2.1;Governing Equations;349
21.1.2.2;Boundary Conditions and Numerical Method;349
21.1.2.3;Grid Configuration;350
21.1.3;Result and Discussion;350
21.1.4;Conclusion;352
21.1.5;References;352
21.2;Pore Scale Simulation of Combustion in Porous Media;354
21.2.1;Introduction;354
21.2.1.1;Test Case;355
21.2.2;Dump Combustor;358
21.2.3;Anderson’s Burner (Hydrogen/Air Combustor);361
21.2.4;Summary;364
21.2.5;References;365
21.3;Combined Finite Element - Particles Discretisation for Simulation of Transport-Dispersion in Porous Media;366
21.3.1;Introduction;366
21.3.2;Finite Element Flow Computation;367
21.3.3;The Streamlines Method;367
21.3.4;Dispersion;369
21.3.5;References;371
22;Part 20 Flow with Non-flat Wall;372
22.1;A Numerical-Asymptotic Method for Computation of Infinite Number of Eddies of Viscous Flows in Domains with Corners;373
22.1.1;Introduction;373
22.1.2;Computational Method;374
22.1.3;Lid-Driven Cavity Problem;375
22.1.4;Conclusion;378
22.1.5;References;378
23;Part 21 Higher-Order Method 1;379
23.1;Implicit High-Order Compact Differencing Methods: Study of Convergence and Stability;380
23.1.1;Introduction;380
23.1.2;Formulation;381
23.1.3;References;385
23.2;A NLFD-Spectral Difference Scheme for Unsteady Flows;386
23.2.1;Introduction;386
23.2.2;Scheme Formulation;386
23.2.3;Numerical Results;388
23.2.3.1;Vortex Advection;388
23.2.3.2;Steady Subsonic Airfoil;389
23.2.3.3;Pitching Subsonic Airfoil;389
23.2.4;Conclusion;391
23.2.5;References;391
24;Part 22 Higher-Order Method 2;392
24.1;High-Order-Accurate Fluctuation Splitting Schemes for Unsteady Hyperbolic Problems Using Lagrangian Elements;393
24.1.1;Introduction;393
24.1.2;Analysis;394
24.1.2.1;Mass Lumping and Explicit Schemes;396
24.1.3;Results;397
24.1.4;References;398
24.2;Assessment of High-Order Algorithms for Aeroacoustic Computation of Shock-Containing Flows;399
24.2.1;Introduction;399
24.2.2;Shock-Capturing Algorithms;400
24.2.3;Test Cases;401
24.2.3.1;Shock Wave Interacting with a Density Disturbance (1D);401
24.2.3.2;Transonic Airfoil (2D);401
24.2.4;Conclusion;403
24.2.5;References;404
24.3;A Dynamic Spatial Filtering Procedure for Shock Capturing in High-Order Computations;405
24.3.1;Introduction;405
24.3.2;Shock-Capturing Methodology;406
24.3.3;Application to a Shock-Propagation Problem;408
24.3.4;Concluding Remarks;409
24.3.5;References;410
24.4;A Discontinuous Galerkin Method Based on a Gas Kinetic Scheme for the Navier-Stokes Equations on Arbitrary Grids;411
24.4.1;Introduction;411
24.4.2;Numerical Method;412
24.4.3;Numerical Examples;413
24.4.4;Conclusions;415
24.4.5;References;416
24.5;Recovery Discontinuous Galerkin Jacobian-Free Newton-Krylov Method for All-Speed Flows;417
24.5.1;Introduction;417
24.5.2;Jacobian-Free Newton-Krylov Framework;417
24.5.3;Recovery Discontinuous Galerkin Method;418
24.5.4;Numerical Examples;420
24.5.5;Conclusion;422
24.5.6;References;422
25;Part 23 Higher-Order Method 3;423
25.1;A Characteristic-Wise Hybrid Compact-WENO Scheme for Solving the Navier-Stokes Equations on Curvilinear Coordinates;424
25.1.1;Introduction;424
25.1.2;Numerical Method;425
25.1.3;Numerical Tests;427
25.1.4;Conclusions;429
25.1.5;References;429
25.2;High-Order Central ENO Finite-Volume Scheme with Adaptive Mesh Refinement for the Advection-Diffusion Equation;430
25.2.1;Scope;430
25.2.2;High-Order CENO Scheme;430
25.2.3;Numerical Results;433
25.2.4;Concluding Remarks;436
25.2.5;References;436
26;Part 24 Hypersonic and Reacting Flows;437
26.1;Active Control of Hypersonic Shock Layer Instability: Direct Numerical Simulation and Experiments;438
26.1.1;Introduction;438
26.1.2;Methods of Investigation;439
26.1.3;Disturbances;439
26.1.3.1;Distributed Receptivity;439
26.1.3.2;Localized Receptivity;440
26.1.4;Active Control;441
26.1.5;References;443
27;Part 25 Immersed Boundary Method/Cartesian Grid Method 1;444
27.1;A Hierarchical Nested Grid Approach for Local Refinement Coupled with an Immersed Boundary Method;445
27.1.1;Introduction;445
27.1.2;Numerical Methodology;446
27.1.2.1;Underlying Numerical Scheme;446
27.1.2.2;Grid Refinement Strategy;447
27.1.3;Results and Discussion;448
27.1.4;Conclusions;450
27.1.5;References;450
27.2;A New Cartesian Grid Method with Adaptive Mesh Refinement for Degenerate Cut Cells on Moving Boundaries;451
27.2.1;Introduction;451
27.2.2;Numerical Methods;451
27.2.2.1;Representation and Tracking of an Irregular Moving Boundary;451
27.2.2.2;Discretization of the Governing Equation;452
27.2.3;Numerical Results;454
27.2.4;Conclusions;456
27.2.5;References;456
27.3;Building-Cube Method for Incompressible Flow Simulations of Complex Geometries;457
27.3.1;Introduction;457
27.3.2;Numerical Method;458
27.3.2.1;Mesh Generation;458
27.3.2.2;Solution Algorithm;458
27.3.3;Numerical Results;459
27.3.3.1;Flow Simulation Around Ahmed Body;459
27.3.3.2;Flow Simulation Around Formula-1 Model;460
27.3.4;Conclusions;461
27.3.5;References;462
28;Part 26 Immersed Boundary Method/Cartesian Grid Method 2;463
28.1;Assessment of Regularized Delta Functions and Feedback Forcing Schemes for an Immersed Boundary Method;464
28.1.1;Introduction;464
28.1.2;Numerical Approach;465
28.1.3;Stability Analysis;466
28.1.4;Results and Discussion;467
28.1.4.1;Stationary Cylinder in a Free-Stream at Re=100;467
28.1.4.2;Transverse Oscillation of a Circular Cylinder;468
28.1.5;Conclusions;469
28.1.6;References;469
28.2;Simulation of a Flow around a Car, Using Cartesian Coordinates;470
28.2.1;Introduction;470
28.2.2;Computational Method;471
28.2.3;Computational Results;474
28.2.4;Conclusion;475
28.2.5;References;475
28.3;Numerical Simulation of Parachute Inflation Process;476
28.3.1;Introduction;476
28.3.2;Numerical Method and Conditions;477
28.3.3;Results;478
28.3.4;Conclusions;481
28.3.5;References;481
28.4;A Finite-Volume Method for Convection Problems with Embedded Moving-Boundaries;482
28.4.1;Introduction;482
28.4.2;Model Equation;483
28.4.2.1;Standard FVM Results;483
28.4.3;Fluxes with Embedded Moving-Boundary Conditions;485
28.4.4;Temporal Discretization;486
28.4.4.1;Monotonicity and Limiters;486
28.4.4.2;Local Adaptivity in Time;487
28.4.5;Results and Conclusion;488
28.4.6;References;488
29;Part 27 Kinetic Approach;489
29.1;Computation of Shock Structure in Diatomic Gases Using the Generalized Boltzmann Equation;490
29.1.1;Introduction;490
29.1.2;Technical Approach;490
29.1.3;Two Level Kinetic Model for RT Relaxation in a Gas;492
29.1.4;Computation of Shock Structure;493
29.1.5;References;495
29.2;A High-Order Accurate Gas-Kinetic BGK Scheme;496
29.2.1;Introduction;496
29.2.2;A High-Order Accurate BGK Scheme;496
29.2.2.1;Fundamental of Gas-Kinetic BGK Scheme;496
29.2.2.2;Extension to High-Order Accuracy;498
29.2.3;Numerical Results;498
29.2.4;Conclusions;500
29.2.5;References;501
30;Part 28 Micro/Nano Fluid Mechanics 1;502
30.1;Numerical Simulations of Three Dimensional Micro Flows;503
30.1.1;Introduction;503
30.1.2;Modeling;503
30.1.2.1;The Stokes Equations for Diphasic Flows in Microfluidic;503
30.1.2.2;The Level Set Method: Parametrization of the Interface;504
30.1.3;The Numerical Method;505
30.1.3.1;The Advection Equation;505
30.1.3.2;The Hydrodynamic Part;505
30.1.4;The Rayleigh-Plateau Instability;505
30.1.4.1;Experimental Considerations;505
30.1.4.2;Jets, Droplets and Plugs;506
30.1.4.3;Discussions;507
30.1.5;The Particular Case of a T-Junction;507
30.1.6;Conclusion;508
30.1.7;References;508
30.2;Optimization of Ribbed Microchannel Heat Sink Using Surrogate Analysis;509
30.2.1;Introduction;509
30.2.2;Problem Description and Numerical Analysis;510
30.2.3;Optimization Procedure;511
30.2.4;Results and Discussion;511
30.2.5;Conclusion;513
30.2.6;References;514
31;Part 29 Micro/Nano Fluid Mechanics 2;515
31.1;Conformations of PMMA Thin Films on an Au (111) Substrate: Chain-Length and Tacticity Effects;516
31.1.1;Introduction;516
31.1.2;Simulation Model;516
31.1.3;Results and Discussion;517
31.1.4;Conclusions;520
31.1.5;References;521
32;Part 30 Multiphase Flow 1;522
32.1;Numerical Method for Flows of Arbitrary Substance in Arbitrary Conditions;523
32.1.1;Introduction;523
32.1.2;Numerical Methods;524
32.1.3;Numerical Examples;525
32.1.4;Conclusion;528
32.1.5;References;528
32.2;Fully-Implicit Interface Tracking for All-Speed Multifluid Flows;529
32.2.1;Introduction;529
32.2.2;Numerical Method (Summary);530
32.2.3;One-Dimensional Tests;531
32.2.4;2D Interface Kinematics by MRD/LS;533
32.2.5;Conclusion;534
32.2.6;References;534
32.3;Development of Surface-Volume Tracking Method Based on MARS;536
32.3.1;Introduction;536
32.3.2;Numerical Method;536
32.3.3;Validation of the Algorithm with Dam Breaking Problem;537
32.3.4;Results and Discussion;539
32.3.5;Conclusion;541
32.3.6;References;541
33;Part 31 Multiphase Flow 2;542
33.1;Adaptive Moment-of-Fluid Method for Multi-Material Flow;543
33.1.1;Backgrounds;543
33.1.2;AMR-MOF;544
33.1.3;Static Interface Reconstruction;545
33.1.4;Dynamic Interface Reconstruction;545
33.1.5;Conclusion;548
33.1.6;References;548
33.2;Numerical Simulation of Underfill Flow in Flip-Chip Packaging;549
33.2.1;Introduction;549
33.2.2;Numerical Simulation of Capillary Flow Undefill;551
33.2.3;Numerical Results;552
33.2.4;Conclusions;554
33.2.5;References;554
33.3;Simulation of Water Advancing over Dry Bed Using Lagrangian Blocks on Eulerian Mesh;555
33.3.1;Introduction;555
33.3.2;LBEM Formulation;557
33.3.3;Friction Effect on Dam-Break Wave;558
33.3.4;Summary of Results Based on $q_{max}$;559
33.3.5;Conclusion;560
33.3.6;References;560
33.4;Time-Derivative Preconditioning for Single and Multicomponent Flows;561
33.4.1;Introduction;561
33.4.2;Governing Equations;562
33.4.3;Numerical Method;562
33.4.3.1;Conservative Formulation;563
33.4.3.2;Nonconservative Formulation;563
33.4.3.3;Hybrid Formulation;563
33.4.4;Results;564
33.4.4.1;Riemann Problems;564
33.4.4.2;NACA0012 Airfoil;565
33.4.4.3;NACA0015 Hydrofoil;566
33.4.5;Summary;566
33.4.6;References;567
34;Part 32 Multiphase Flow 3;568
34.1;High-Speed Jet Formation after Solid Object Impact;569
34.1.1;Introduction;569
34.1.2;Methods;569
34.1.3;Results;570
34.1.4;Conclusions;572
34.1.5;References;572
34.2;Numerical Study on Population Balance Approaches in Modeling of Isothermal Vertical Bubbly Flows;573
34.2.1;Introduction;573
34.2.2;Mathematical Models;574
34.2.2.1;Population Balance Approaches;575
34.2.3;Numerical Details;575
34.2.4;Results and Discussions;576
34.2.5;Conclusions;578
34.2.6;References;578
34.3;Direct Numerical Simulation of Cavitation Noise for a 3D Circular Cylinder Cross-Flow;579
34.3.1;Introduction;579
34.3.2;Computational Methods ;580
34.3.2.1;Density-Based Homogeneous Equilibrium Model;580
34.3.2.2;Selective Spatial Filtering;581
34.3.3;Results and Discussion;582
34.3.4;Summary and Conclusions;584
34.3.5;References;584
34.4;Numerical Method for Shock-Cavitation Bubble Interaction Problems;585
34.4.1;Introduction;585
34.4.2;Homogeneous Cavitation Model;586
34.4.3;Numerical Method;586
34.4.4;Numerical Results;588
34.4.5;Conclusions;590
34.4.6;References;590
35;Part 33 Optimization 1;591
35.1;A Low Dissipative Discrete Adjoint m-KFVS Method;592
35.1.1;Introduction;592
35.1.2;m-KFVS Method;593
35.1.3;Optimal Control of Numerical Dissipation;594
35.1.4;References;597
35.2;Second Order Sensitivities for Shape Optimization in the Presence of Shocks;598
35.2.1;Introduction;598
35.2.2;Problem Definition;599
35.2.3;Direct and Adjoint Based Methods for Hessian Computation;600
35.2.4;Numerical Test Demonstrating the Impact of the Hessian on Convergence of Transonic Optimal Design;601
35.2.5;References;604
35.3;Strategies for Robust Convergence Characteristics of Discrete Adjoint Method;605
35.3.1;Introduction;605
35.3.2;Sensitivity Analysis via Volume Integrated Functions;605
35.3.3;Enhancement of Diagonal Dominance of Adjoint Matrix;607
35.3.4;Conclusion;611
35.3.5;References;611
35.4;On the Reliability of the Aerodynamic Analysis Using a Moment Method;612
35.4.1;Introduction;612
35.4.2;Reliability Analysis;613
35.4.2.1;Monte Carlo Simulation;613
35.4.2.2;First Order Reliability Method;613
35.4.2.3;Moment Method;614
35.4.3;Flow Analysis;614
35.4.4;Reliability of Flow Analysis;615
35.4.4.1;2D Airfoil;615
35.4.4.2;3D Wing;615
35.4.5;Conclusion;616
35.4.6;References;616
36;Part 34 Optimization 2;618
36.1;Uncertainty Based MDO of UAS Using HAPMOEA;619
36.1.1;Introduction;619
36.1.2;Methodology;620
36.1.3;Real World Design Problem;620
36.1.4;Conclusions;624
36.1.5;References;624
36.2;The Optimum Design of a Propeller Energy-Saving Device by Computational Fluid Dynamics;625
36.2.1;Introduction;625
36.2.2;Geometric Parameters;625
36.2.3;Parametric Analysis;626
36.2.4;Computational Results;627
36.2.5;Conclusions;629
36.2.6;References;630
37;Part 35 Rotor Aerodynamics;631
37.1;An Analysis on the Helicopter Rotor Aerodynamics in Hover and Forward Flight Using CFD/Time-Marching-Free-Wake Coupling Method;632
37.1.1;Introduction;632
37.1.2;Methodology;633
37.1.2.1;Numerical Method;633
37.1.3;Numerical Results;635
37.1.4;Conclusion;637
37.1.5;References;637
38;Part 36 Turbulence Modeling and Simulation 1;638
38.1;Stochastic-Determinism Approach for Simulating the Transition Points in Internal Flows with Various Inlet Disturbances;639
38.1.1;Introduction;639
38.1.2;Governing Equation and Numerical Method;639
38.1.3;Computational Results;641
38.1.4;Conclusion;644
38.1.5;References;644
38.2;Investigation of an Anisotropic NS-a Model for Wall-Bounded Flows;645
38.2.1;Introduction;645
38.2.2;Model Formulation;645
38.2.3;Description of the Test Cases;647
38.2.4;Results;648
38.2.5;References;650
38.3;Computing Turbulent Flows Using Meshless Solver LSFD-U;651
38.3.1;Introduction;651
38.3.2;LSFD-U;652
38.3.3;Point Generation;653
38.3.4;LSFD-U Flow Solver;653
38.3.5;Numerical Results;654
38.3.6;Conclusions;656
38.3.7;References;657
38.4;Parallel Adaptive Mesh Refinement Scheme for LES of Turbulent Premixed Flames;658
38.4.1;Introduction and Scope;658
38.4.2;LES Modelling;658
38.4.3;Thickened Flame Model;659
38.4.4;Flame Surface Density Model;660
38.4.5;Parallel Implicit AMR Finite-Volume Scheme;661
38.4.6;Numerical Results;662
38.4.7;Conclusions;664
38.4.8;References;664
39;Part 37 Turbulence Modeling and Simulation 2;665
39.1;The Characteristic Analysis of Fire-Driven Flow Simulation Code (FDS) for Railway Tunnel;666
39.1.1;Introduction;666
39.1.2;Flow Conditions and Numerical Method;667
39.1.2.1;Flow Conditions;667
39.1.2.2;Grid Generation;668
39.1.2.3;Governing Equation;668
39.1.2.4;Numerical Method;669
39.1.3;Results and Discussion;669
39.1.4;Conclusion;671
39.1.5;References;672
40;Part 38 Upwind Scheme 1;673
40.1;Discontinuous Fluctuation Distribution for Time-Dependent Problems;674
40.1.1;Introduction;674
40.1.2;Discontinuous Fluctuation Distribution;675
40.1.2.1;Time-Dependent Problems;676
40.1.2.2;One Space Dimension;677
40.1.3;Numerical Results;678
40.1.4;Summary;679
40.1.5;References;679
40.2;Weighted Compact Schemes for Shock / Boundary Layer Interaction;680
40.2.1;Introduction;680
40.2.2;Hybrid Weighted Compact-ENO Scheme;681
40.2.3;Weighted Compact – ENO for Incident Shock / Boundary Layer Interaction;682
40.2.3.1;Numerical Girds for the Main Flow Solver;682
40.2.3.2;Initial and Boundary Conditions for the Main Flow Solver;683
40.2.3.3;Preliminary Numerical Results (Scaled by a Factor of 3 in y-Direction);683
40.2.4;Concluding Remarks;685
40.2.5;References;685
40.3;The Riemann Problem for Reynolds-Stress-Transport in RANS and VLES;686
40.3.1;Introduction;686
40.3.2;Reynolds-Stress Transport;687
40.3.2.1;The Complete Set of Equations;687
40.3.2.2;Eigenvalues and Eigenvectors;688
40.3.2.3;Approximate Jump Relations;688
40.3.2.4;Approximate Jump Relations for $\lambda \neq \~{u}$;689
40.3.2.5;Approximate Jump Relations for $\lambda = \~{u}$;690
40.3.2.6;Closure Relations for the {\sc hllc–rsm} Flux;690
40.3.3;References;691
41;Part 39 Upwind Scheme 2;693
41.1;Improving Monotonicity of the 2nd Order Backward Difference Time Integration Scheme by Temporal Limiting;694
41.1.1;Blending Coeficient;695
41.1.2;Results;697
41.1.3;References;699
41.2;The Finite Volume Local Evolution Galerkin Method for Solving the Euler Equations;700
41.2.1;Introduction;700
41.2.2;Numerical Methods;701
41.2.2.1;A Comparison between the FVEG and FVLEG Methods;701
41.2.2.2;The Approximate Evolution Operators for the FVLEG Scheme;703
41.2.3;Numerical Results;705
41.2.4;Conclusions;706
41.2.5;References;706
41.3;Time-Implicit Approximation of the Multi-pressure Gas Dynamics Equations in Several Space Dimensions;707
41.3.1;Introduction;707
41.3.2;A Tractable Equivalent Reformulation;708
41.3.3;Numerical Approximation;710
41.3.4;Numerical Illustration;712
41.3.5;References;712
41.4;Smoothness Monitors for Compressible Flow Computation;713
41.4.1;Redundant Wavelets;713
41.4.2;Test Cases;716
41.4.3;References;719
42;Part 40 Wake Flow;720
42.1;Proper Orthogonal Decomposition of Unsteady Heat Transfer from Staggered Cylinders at Moderate Reynolds Numbers;721
42.1.1;Introduction;721
42.1.2;Computational Details;722
42.1.3;Results and Discussion;723
42.1.3.1;Flow and Heat Transfer Characteristics;723
42.1.3.2;Proper Orthogonal Decomposition;724
42.1.4;Summary;726
42.1.5;References;726
42.2;Effect of Rotation Rates and Gap Spacing on the Structure of Low Reynolds Number Flow over Two Rotating Circular Cylinders;728
42.2.1;Introduction;728
42.2.2;Governing Equations and Numerical Methods;728
42.2.3;Results;730
42.2.4;References;734
42.3;Improvement of Reduced Order Modeling Based on POD;735
42.3.1;Introduction;735
42.3.2;A Pressure Extended Reduced Order Model;736
42.3.3;Stabilization of Reduced Order Models;737
42.3.3.1;Residuals Based Stabilization Method: Model B$^{[N_{r};K]$;737
42.3.3.2;SUPG and VMS Methods: Models C$^{[N_{r}]$ and D$^{[N_{r}]}$;737
42.3.3.3;Results of Stabilization Methods;738
42.3.4;Improvement of the Functional Subspace;738
42.3.5;Conclusions;739
42.3.6;References;740
43;Part 41 Technical Notes;741
43.1;Poster Session - MP1;17
43.1.1;Modelling and Simulation of Droplet Distribution from Entrained Liquid Film in Gas-Liquid Systems;742
43.1.1.1;References;743
43.1.2;The Effect of the Number of Computational Grids on Calculation Results of Co-axial Jet Flows by Large Eddy Simulation Using Dynamic SGS Model;744
43.1.2.1;Introduction;744
43.1.2.2;Numerical Calculation;744
43.1.2.3;Results;745
43.1.2.4;References;745
43.1.3;Development and Application of the Collocations and Least Squares Method;746
43.1.4;Combined Experimental and Numerical Analysis of Incompressible Flow around an Airfoil;748
43.1.4.1;Introduction;748
43.1.4.2;Numerical Method;749
43.1.4.3;Experimental Apparatus;749
43.1.4.4;Results and Discussions;750
43.1.4.5;Conclusion;753
43.1.4.6;References;753
43.1.5;CFD Simulation of Gas-Water Two-Phase Flow in Turbocharger;754
43.1.6;Numerical Analysis of Optical Systems for Compressible Flow Visualization;756
43.1.6.1;Introduction;756
43.1.6.2;Optical Systems;757
43.1.6.3;Simulation Techniques;757
43.1.6.3.1;CFD;757
43.1.6.3.2;Ray-Tracing Method;758
43.1.6.3.3;Adaptive Ray-Tracing Method;759
43.1.6.4;Results;759
43.1.6.5;Conclusions;759
43.1.6.6;References;759
43.2;Poster Session - TuP1;18
43.2.1;Application of a DRP Upwinding Scheme in Immersed Boundary Method;760
43.2.1.1;Mimic Interpolation Immersed Boundary Method;760
43.2.1.2;Dispersion-Relation-Preserving Scheme;761
43.2.2;Convergence Acceleration Method for Linear Iterative Process;763
43.2.2.1;References;764
43.2.3;Heat Transfer Correlations and Pressure Drop for Cross-Cut Heat Sinks Using CFD: Technical Notes;765
43.2.3.1;Introduction;765
43.2.3.2;Numerical Results and Conclusions;765
43.2.3.3;References;766
43.2.4;CFD Study of Traveling Wave within a Piston-Less Striling Heat Engine;767
43.2.4.1;Introduction;767
43.2.4.2;Results and Discussions;768
43.2.4.3;References;768
43.2.5;Numerical Simulation of Acoustic Waves in Jet Flows;769
43.2.5.1;Introduction;769
43.2.5.2;Experimental Results;769
43.2.5.3;Numerical Results;769
43.2.5.4;References;770
43.2.6;Robust BEM Solver for Sound Scattering;771
43.2.6.1;References;772
44;Author Index;773




