Sanjiva Lele
Professor of Aeronautics and Astronautics and of Mechanical Engineering
Bio
Professor Lele's research combines numerical simulations with modeling to study fundamental unsteady flow phemonema, turbulence, flow instabilities, and flow-generated sound. Recent projects include shock-turbulent boundary layer interactions, supersonic jet noise, wind turbine aeroacoustics, wind farm modeling, aircraft contrails, multi-material mixing and multi-phase flows involving cavitation. He is also interested in developing high-fidelity computational methods for engineering applications.
Academic Appointments
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Professor, Aeronautics and Astronautics
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Professor, Mechanical Engineering
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Member, Bio-X
Honors & Awards
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Stanford Asian American Faculty Award, Stanford Asian American Faculty
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Stanford University Fellow, Stanford University
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American Physical Society NSF Presidential Young Investigator RT Knapp Best Paper Award, American Physical Society
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ASME Best Student Paper Award (with T. Manning), AIAA F.N. Frenkeil Award, ASME
Professional Education
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PhD, Cornell, Mechanical Engineering (1985)
2015-16 Courses
- Advanced Topics in Turbulence
ME 461 (Aut) - Fundamentals of Acoustics
AA 201A (Spr) - Partial Differential Equations in Engineering
CME 204, ME 300B (Win) - Seminar in Fluid Mechanics
ENGR 298 (Aut) -
Independent Studies (13)
- Directed Research and Writing in Aero/Astro
AA 190 (Aut, Win, Spr, Sum) - Engineering Problems
ME 391 (Aut, Win, Spr, Sum) - Engineering Problems and Experimental Investigation
ME 191 (Aut, Win, Spr, Sum) - Experimental Investigation of Engineering Problems
ME 392 (Aut, Win, Spr, Sum) - Honors Research
ME 191H (Aut, Win, Spr, Sum) - Independent Study in Aero/Astro
AA 199 (Aut, Win, Spr, Sum) - Master's Research
CME 291 (Aut, Win, Spr, Sum) - Ph.D. Research
CME 400 (Aut, Win, Spr, Sum) - Ph.D. Teaching Experience
ME 491 (Aut, Win, Spr, Sum) - Practical Training
AA 291 (Sum) - Practical Training
ME 299A (Aut, Win, Spr, Sum) - Practical Training
ME 299B (Aut, Win, Spr, Sum) - Problems in Aero/Astro
AA 290 (Aut, Win, Spr, Sum)
- Directed Research and Writing in Aero/Astro
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Prior Year Courses
2014-15 Courses
- Advanced Fluid Mechanics Flow Instability
ME 451B (Aut) - Partial Differential Equations in Engineering
CME 204, ME 300B (Win) - Seminar in Fluid Mechanics
ENGR 298 (Win) - Topics in Aeroacoustics
AA 201B (Spr)
2013-14 Courses
- Advanced Topics in Turbulence
ME 461 (Aut) - Fundamentals of Acoustics
AA 201A (Spr) - Partial Differential Equations in Engineering
CME 204, ME 300B (Win)
2012-13 Courses
- Advanced Fluid Mechanics
ME 451B (Aut) - Partial Differential Equations in Engineering
CME 204, ME 300B (Win) - Topics in Aeroacoustics
AA 201B (Spr)
- Advanced Fluid Mechanics Flow Instability
Stanford Advisees
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Doctoral Dissertation Advisor (AC)
Aditya Ghate -
Postdoctoral Research Mentor
Niranjan Ghaisas
All Publications
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Study of supertonic wave components in high-speed turbulent jets using an LES database
JOURNAL OF SOUND AND VIBRATION
2014; 333 (25): 6900-6923
View details for DOI 10.1016/j.jsv2014.08.004
View details for Web of Science ID 000343337900009
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Parameterization of Boundary-Layer Transition Induced by Isolated Roughness Elements
AIAA JOURNAL
2014; 52 (10): 2261-2269
View details for DOI 10.2514/1.J052842
View details for Web of Science ID 000342759200013
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On the Richtmyer-Meshkov instability evolving from a deterministic multimode planar interface
JOURNAL OF FLUID MECHANICS
2014; 755
View details for DOI 10.1017/jfm.2014.436
View details for Web of Science ID 000341128600025
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A second golden age of aeroacoustics?
PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES
2014; 372 (2022)
Abstract
In 1992, Sir James Lighthill foresaw the dawn of a second golden age in aeroacoustics enabled by computer simulations (Hardin JC, Hussaini MY (eds) 1993 Computational aeroacoustics, New York, NY: Springer (doi:10.1007/978-1-4613-8342-0)). This review traces the progress in large-scale computations to resolve the noise-source processes and the methods devised to predict the far-field radiated sound using this information. Keeping focus on aviation-related noise sources a brief account of the progress in simulations of jet noise, fan noise and airframe noise is given highlighting the key technical issues and challenges. The complex geometry of nozzle elements and airframe components as well as the high Reynolds number of target applications require careful assessment of the discretization algorithms on unstructured grids and modelling compromises. High-fidelity simulations with 200-500 million points are not uncommon today and are used to improve scientific understanding of the noise generation process in specific situations. We attempt to discern where the future might take us, especially if exascale computing becomes a reality in 10 years. A pressing question in this context concerns the role of modelling in the coming era. While the sheer scale of the data generated by large-scale simulations will require new methods for data analysis and data visualization, it is our view that suitable theoretical formulations and reduced models will be even more important in future.
View details for DOI 10.1098/rsta.2013.0321
View details for Web of Science ID 000338844700006
View details for PubMedID 25024417
- Direct Simulation of a Mach 1.92 Jet and its Sound Field
- Direct Simulation and Analysis of Shock-turbulence Interaction
- Evaluation of far-field sound using open surface corrections to Lighthill’s equation
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Large-Eddy Simulations of a Normal Shock Train in a Constant-Area Isolator
AIAA JOURNAL
2014; 52 (3): 539-558
View details for DOI 10.2514/1.J052348
View details for Web of Science ID 000337796100007
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Effect of adverse pressure gradient on high speed boundary layer transition
PHYSICS OF FLUIDS
2014; 26 (2)
View details for DOI 10.1063/1.4864337
View details for Web of Science ID 000332322000025
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Numerical investigation of turbulence in reshocked Richtmyer-Meshkov unstable curtain of dense gas
SHOCK WAVES
2014; 24 (1): 79-95
View details for DOI 10.1007/s00193-013-0478-z
View details for Web of Science ID 000331656400010
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Effects of mean flow convection, quadrupole sources and vortex shedding on airfoil overall sound pressure level
JOURNAL OF SOUND AND VIBRATION
2013; 332 (26): 6905-6912
View details for DOI 10.1016/j.jsv.2013.08.029
View details for Web of Science ID 000328012600001
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Effects of plume-scale versus grid-scale treatment of aircraft exhaust photochemistry
GEOPHYSICAL RESEARCH LETTERS
2013; 40 (21): 5815-5820
View details for DOI 10.1002/2013GL057665
View details for Web of Science ID 000327810800045
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Fast acoustic scattering predictions with non-uniform potential flow effects
JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING
2013; 35 (4): 407-418
View details for DOI 10.1007/s40430-013-0038-6
View details for Web of Science ID 000324128000007
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A mechanism for unsteady separation in over-expanded nozzle flow
PHYSICS OF FLUIDS
2013; 25 (11)
View details for DOI 10.1063/1.4819349
View details for Web of Science ID 000329184100010
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Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers
JOURNAL OF FLUID MECHANICS
2013; 730: 491-532
View details for DOI 10.1017/jfm.2013.350
View details for Web of Science ID 000324270200007
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Flow physics and RANS modelling of oblique shock/turbulent boundary layer interaction
JOURNAL OF FLUID MECHANICS
2013; 729: 231-284
View details for DOI 10.1017/jfm.2013.301
View details for Web of Science ID 000322379400011
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Directional artificial fluid properties for compressible large-eddy simulation
JOURNAL OF COMPUTATIONAL PHYSICS
2013; 246: 207-220
View details for DOI 10.1016/j.jcp.2013.03.026
View details for Web of Science ID 000320604000013
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Turbulent kinetic energy spectra of solar convection from New Solar Telescope observations and realistic magnetohydrodynamic simulations
PHYSICA SCRIPTA
2013; T155
View details for DOI 10.1088/0031-8949/2013/T155/014025
View details for Web of Science ID 000321863000027
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UBIQUITOUS SOLAR ERUPTIONS DRIVEN BY MAGNETIZED VORTEX TUBES
ASTROPHYSICAL JOURNAL
2013; 770 (1)
View details for DOI 10.1088/0004-637X/770/1/37
View details for Web of Science ID 000319986400037
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Crackle Noise in Heated Supersonic Jets
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME
2013; 135 (5)
View details for DOI 10.1115/1.4007867
View details for Web of Science ID 000326154200002
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Reynolds- and Mach-number effects in canonical shock-turbulence interaction
JOURNAL OF FLUID MECHANICS
2013; 717: 293-321
View details for DOI 10.1017/jfm.2012.573
View details for Web of Science ID 000314423900012
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On the use of the Ffowcs Williams-Hawkings equation to predict far-field jet noise from large-eddy simulations
INTERNATIONAL JOURNAL OF AEROACOUSTICS
2013; 12 (1-2): 1-20
View details for DOI 10.1260/1475-472X.12.1-2.1
View details for Web of Science ID 000317568200001
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The effects of aircraft on climate and pollution. Part II: 20-year impacts of exhaust from all commercial aircraft worldwide treated individually at the subgrid scale
FARADAY DISCUSSIONS
2013; 165: 369-382
View details for DOI 10.1039/c3fd00034f
View details for Web of Science ID 000329068600019
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The effects of aircraft on climate and pollution, Part II: 20-year impacts of exhaust from all commercial aircraft worldwide treated individually at the subgrid scale
Faraday Discuss.
2013
View details for DOI 10.1039/C3FD00034F
- Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers J. Fluid Mech. 2013; 730: 491-532
- Towards full-scale numerical simulations of travelling-wave thermoacoustic Stirling engines 2013
- Flow physics and RANS modeling of oblique shock/turbulent boundary layer interaction J. Fluid Mech. 2013; 729: 231-284
- Towards full-scale numerical simulations of travelling-wave thermoacoustic Stirling engines 2013
- Assessment of wall-modeled large-eddy simulation for supersonic compression ramp flows 2013
- A probabilistic ice habit model for LES of contrails 2013
- Simulations of a normal shock train in a constant area duct using wall-modeled LES 2013
- A mechanism for unsteady separation in over-expanded nozzle flow Phys. Fluids. 2013; 25 (11): 110809
- Effects of Mean Flow Convection, Quadrupole sources and vortex shedding on airfoil overall sound pressure level J. Sound and Vib., to appear. 2013
- Directional artificial fluid properties for compressible large-eddy simulations J. Comput. Phys. 2013; 246: 207-220
- The source of crackle noise in heated supersonic jets 2013
- Nozzle wall modeling in unstructured large-eddy simulations for hot supersonic jet predictions 2013
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Ovarian Cancer, Version 3.2012 Featured Updates to the NCCN Guidelines
JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK
2012; 10 (11): 1339-1349
View details for Web of Science ID 000310822900005
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Trailing-Edge Noise Predictions Using Compressible Large-Eddy Simulation and Acoustic Analogy
AIAA JOURNAL
2012; 50 (11): 2423-2434
View details for DOI 10.2514/1.J051638
View details for Web of Science ID 000310559000011
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Convective effects and the role of quadrupole sources for aerofoil aeroacoustics
JOURNAL OF FLUID MECHANICS
2012; 708: 502-538
View details for DOI 10.1017/jfm.2012.327
View details for Web of Science ID 000308989800021
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Interaction of a converging spherical shock wave with isotropic turbulence
PHYSICS OF FLUIDS
2012; 24 (8)
View details for DOI 10.1063/1.4737892
View details for Web of Science ID 000308417000035
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Vortex tubes of turbulent solar convection
PHYSICA SCRIPTA
2012; 86 (1)
View details for DOI 10.1088/0031-8949/86/01/018403
View details for Web of Science ID 000306245200033
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Large-Eddy Simulations of Perfectly Expanded Supersonic Jets Using an Unstructured Solver
AMER INST AERONAUTICS ASTRONAUTICS. 2012: 1103-1118
View details for DOI 10.2514/1.J051211
View details for Web of Science ID 000303365700010
- Investigation of bubble-bubble interaction and shock-reflection in homogeneous bubbly flow 2012
- Effects of Mean Flow Convection and Quadrupole Sources on Airfoil Trailing Edge Noise 2012
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CRACKLE NOISE IN HEATED SUPERSONIC JETS
PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 1
2012: 337-345
View details for Web of Science ID 000335720700032
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Interaction of converging spherical shock wave with isotropic turbulence
Physics of Fluids
2012; 24 (8): 21
View details for DOI 10.1063/1.4737892
- Large-eddy simulation for supersonic rectangular jet noise prediction: effects of chevrons 2012
- Investigation of Noise Generated by a DU96 Airfoil 2012
- Large-eddy and RANS simulations of normal shock train in a constant area isolator 2012
- Large-eddy simulation of perfectly expanded supersonic jets using unstructured solver AIAA J. 2012; 50: 1103-1118
- Low Frequency Unsteadiness in Nozzle Flow Separation 2012
- Aeroacoustics of a supersonic rectangular jet: experiments and LES predictions 2012
- Quadrupole Noise in Turbulent Wake Interaction Problems 2012
- Towards Best Practices for Jet Noise Predictions with Unstructured Large Eddy Simulations 2012
- Crackle noise in heated supersonic jets 2012
- Crackle noise in heated supersonic jets J. Eng. Gas Turbines & Power, GTP-12-1155. 2012
- Unstructured Large Eddy Simulation of a Hot Supersonic Over-Expanded Jet with Chevrons 2012
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Directional artificial bulk viscosity for shock capturing on high aspect ratio grids
Comput. Science & Discovery
2012; 5: 14008
View details for DOI 10.1088/1749-4699/5/1/014008
- Effects of heating on noise radiation from turbulent mixing layers with initially laminar and turbulent boundary layers 2012
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Wideband fast multipole boundary element method: Application to acoustic scattering from aerodynamic bodies
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS
2011; 67 (12): 2108-2129
View details for DOI 10.1002/fld.2486
View details for Web of Science ID 000297736100020
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Non-normal global modes of high-speed jets
INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS
2011; 3 (4): 285-301
View details for DOI 10.1260/1756-8277.3.4.285
View details for Web of Science ID 000304911100003
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Large eddy simulations of contrail development: Sensitivity to initial and ambient conditions over first twenty minutes
JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES
2011; 116
View details for DOI 10.1029/2011JD015806
View details for Web of Science ID 000297266900002
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Nonlinear effects in the combined Rayleigh-Taylor/Kelvin-Helmholtz instability
PHYSICS OF FLUIDS
2011; 23 (11)
View details for DOI 10.1063/1.3660723
View details for Web of Science ID 000297939200026
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Vertical mixing of commercial aviation emissions from cruise altitude to the surface
JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES
2011; 116
View details for DOI 10.1029/2010JD015532
View details for Web of Science ID 000293091100009
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Aeroacoustic Integrals Accelerated by Fast Multipole Method
AIAA JOURNAL
2011; 49 (7): 1466-1477
View details for DOI 10.2514/1.J050861
View details for Web of Science ID 000293113500014
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The effects of aircraft on climate and pollution. Part I: Numerical methods for treating the subgrid evolution of discrete size- and composition-resolved contrails from all commercial flights worldwide
JOURNAL OF COMPUTATIONAL PHYSICS
2011; 230 (12): 5115-5132
View details for DOI 10.1016/j.jcp.2011.03.031
View details for Web of Science ID 000291125400040
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Sound generation due to unsteady motion of a cylinder
PHYSICS OF FLUIDS
2011; 23 (4)
View details for DOI 10.1063/1.3579489
View details for Web of Science ID 000290050000038
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Improving Low-Frequency Characteristics of Recycling/Rescaling Inflow Turbulence Generation
AIAA JOURNAL
2011; 49 (3): 582-597
View details for DOI 10.2514/1.J050705
View details for Web of Science ID 000288059200012
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Interaction of a Taylor blast wave with isotropic turbulence
PHYSICS OF FLUIDS
2011; 23 (3)
View details for DOI 10.1063/1.3560384
View details for Web of Science ID 000289153000028
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Two-dimensional viscous flow simulation of a shock accelerated heavy gas cylinder
PHYSICS OF FLUIDS
2011; 23 (2)
View details for DOI 10.1063/1.3553282
View details for Web of Science ID 000287812800022
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Global modes and transient response of a cold supersonic jet
JOURNAL OF FLUID MECHANICS
2011; 669: 225-241
View details for DOI 10.1017/S0022112010005380
View details for Web of Science ID 000287935200011
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Epithelial Ovarian Cancer
JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK
2011; 9 (1): 82-113
View details for Web of Science ID 000287217200008
View details for PubMedID 21233246
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NOISE PREDICTION OF PRESSURE-MISMATCHED JETS USING UNSTRUCTURED LARGE EDDY SIMULATION
PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 1
2011: 381-387
View details for Web of Science ID 000320677300034
- Effects of heating on noise radiation from a two-dimensional mixing layer: direct computation and acoustic analogy predictions 2011
- Large eddy simulation of an over-expanded planar nozzle 2011
- High-fidelity large-eddy simulation for supersonic rectangular jet noise prediction 2011
- Large eddy simulation of a Mach 2.9 turbulent boundary layer over a 24 deg compression ramp 2011
- Analysis and correction of errors generated by slowly moving shocks 2011
- Large eddy simulation of persistent aircraft contrails 2011
- Unstructured large-eddy simulation for prediction of noise issued from turbulent jets in various configurations 2011
- Direct simulation of transition and heat-transfer overshoot in a Mach 6 flat plate boundary layer 2011
- LES of tripped super-critical cylinder flow: towards tandem cylinder noise prediction 2011
- Trailing edge noise predictions using compressible LES and acoustic analogy 2011
- Heat transfer prediction in high pressure turbine cascade with free-stream turbulence using LES 2011
- A parametric investigation of oblique shockwave/turbulent boundary layer interaction using LES 2011
- Large-eddy simulation of supersonic, turbulent mixing layers downstream of a splitter plate 2011
- Effect of aircraft on climate and pollution. Part I: Numerical methods for treating the subgrid evolution of discrete size- and composition-resolved contrails from all commerical flights worldwide J. Computational Phys. 2011; 230 (12): 5115-5132
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Cervical Cancer Screening
JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK
2010; 8 (12): 1358-1386
View details for Web of Science ID 000285132200006
View details for PubMedID 21147902
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Acoustic Analogy Formulations Accelerated by Fast Multipole Method for Two-Dimensional Aeroacoustic Problems
AIAA JOURNAL
2010; 48 (10): 2274-2285
View details for DOI 10.2514/1.J050338
View details for Web of Science ID 000282675700010
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Large-Eddy Simulation of Jet Mixing in Supersonic Crossflows
AMER INST AERONAUT ASTRONAUT. 2010: 2063-2083
View details for DOI 10.2514/1.J050282
View details for Web of Science ID 000281548100018
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Investigation and modeling of bubble-bubble interaction effect in homogeneous bubbly flows
PHYSICS OF FLUIDS
2010; 22 (6)
View details for DOI 10.1063/1.3432503
View details for Web of Science ID 000280143100015
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Large eddy simulation of free-stream turbulence effects on heat transfer to a high-pressure turbine cascade
JOURNAL OF TURBULENCE
2010; 11 (6): 1-15
View details for DOI 10.1080/14685241003705756
View details for Web of Science ID 000275858900001
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Assessment of localized artificial diffusivity scheme for large-eddy simulation of compressible turbulent flows
JOURNAL OF COMPUTATIONAL PHYSICS
2010; 229 (5): 1739-1762
View details for DOI 10.1016/j.jcp.2009.11.005
View details for Web of Science ID 000274309700019
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Assessment of high-resolution methods for numerical simulations of compressible turbulence with shock waves
JOURNAL OF COMPUTATIONAL PHYSICS
2010; 229 (4): 1213-1237
View details for DOI 10.1016/j.jcp.2009.10.028
View details for Web of Science ID 000274547000013
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Compact adaptive-grid scheme for high numerical resolution simulations of isotachophoresis
JOURNAL OF CHROMATOGRAPHY A
2010; 1217 (4): 588-599
Abstract
In a previous publication we demonstrated a fast simulation tool for solution of electrophoretic focusing and separation. We here describe the novel mathematical model and numerical algorithms used to create this code. These include the representation of advection-diffusion equations on an adaptive grid, high-resolution discretization of the equations (sixth order compact), a new variational-based approach for controlling the motion of grid points, and new boundary conditions which enable solution in a moving frame of reference. We discuss the advantages of combining a high-resolution discretization with an adaptive grid in accurately resolving sharp interfaces in isotachophoresis, and provide verification against known analytical solutions and comparison with prevailing exiting numerical algorithms.
View details for DOI 10.1016/j.chroma.2009.11.072
View details for Web of Science ID 000274479200020
View details for PubMedID 20022605
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Effect of transport modeling on hypersonic cooled wall boundary layer stability
SPRINGER. 2010: 489-492
View details for DOI 10.1007/978-90-481-3723-7_82
View details for Web of Science ID 000277097200082
- Large-eddy simulations of perfectly-expanded supersonic jets: quality assessment and validation 2010
- Large eddy simulation of an oblique shock impinging on a turbulent boundary layer 2010
- Numerical simulation of multicomponent shock accelerated flows and mixing using localized artificial diffusivity method 2010
- Far-field filtering and source-imaging for the study of jet noise 2010
- Fast acoustic scattering simulations with non-uniform potential flow effects 2010
- Parameterization of subgrid aircraft emission plumes for use in large-scale atmospheric simulations Atmos. Chem. Phys., also ATMOS. CHEM. PHYS. DISCUSS. 2010, 2009; 10, 9: 2551-2560, 24755–24781
- Effect of chemistry modeling on hypersonic boundary layer linear stability prediction 2010
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Parameterization of subgrid plume dilution for use in large-scale atmospheric simulations
ATMOSPHERIC CHEMISTRY AND PHYSICS
2010; 10 (5): 2551-2560
View details for Web of Science ID 000275505500031
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Analysis of emission data from global commercial aviation: 2004 and 2006
ATMOSPHERIC CHEMISTRY AND PHYSICS
2010; 10 (13): 6391-6408
View details for DOI 10.5194/acp-10-6391-2010
View details for Web of Science ID 000279851400043
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UNSTRUCTURED LARGE EDDY SIMULATION TECHNOLOGY FOR PREDICTION AND CONTROL OF JET NOISE
PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 1
2010: 57-70
View details for Web of Science ID 000290692000007
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Sources of high-speed jet noise: analysis of LES data and modeling
ELSEVIER SCIENCE BV. 2010: 84-93
View details for DOI 10.1016/j.proeng.2010.09.010
View details for Web of Science ID 000287141600010
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Direct numerical simulation of canonical shock/turbulence interaction
PHYSICS OF FLUIDS
2009; 21 (12)
View details for DOI 10.1063/1.3275856
View details for Web of Science ID 000273216700027
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The dynamics of nonlinear instability waves in laminar heated and unheated compressible mixing layers
PHYSICS OF FLUIDS
2009; 21 (9)
View details for DOI 10.1063/1.3232329
View details for Web of Science ID 000270378600033
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A modified artificial viscosity approach for compressible turbulence simulations
JOURNAL OF COMPUTATIONAL PHYSICS
2009; 228 (14): 4965-4969
View details for DOI 10.1016/j.jcp.2009.04.009
View details for Web of Science ID 000267846500001
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On the growth and propagation of linear instability waves in compressible turbulent jets
PHYSICS OF FLUIDS
2009; 21 (5)
View details for DOI 10.1063/1.3139302
View details for Web of Science ID 000266500500029
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Linear and nonlinear processes in two-dimensional mixing layer dynamics and sound radiation
JOURNAL OF FLUID MECHANICS
2009; 625: 321-351
View details for DOI 10.1017/S0022112008005715
View details for Web of Science ID 000265801400012
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Open source simulation tool for electrophoretic stacking, focusing, and separation
JOURNAL OF CHROMATOGRAPHY A
2009; 1216 (6): 1008-1018
Abstract
We present the development, formulation, and performance of a new simulation tool for electrophoretic preconcentration and separation processes such as capillary electrophoresis, isotachophoresis, and field amplified sample stacking. The code solves the one-dimensional transient advection-diffusion equations for multiple multivalent weak electrolytes (including ampholytes) and includes a model for pressure-driven flow and Taylor-Aris dispersion. The code uses a new approach for the discretization of the equations, consisting of a high resolution compact scheme which is combined with an adaptive grid algorithm. We show that this combination allows for accurate resolution of sharp concentration gradients at high electric fields, while at the same time significantly reducing the computational time. We demonstrate smooth, stable, and accurate solutions at current densities as high as 5000A/m(2) using only 300 grid points, and a 75-fold reduction in computational time compared with equivalent uniform grid techniques. The code is available as an open source for free at http://microfluidics.stanford.edu.
View details for DOI 10.1016/j.chroma.2008.12.022
View details for Web of Science ID 000263087700017
View details for PubMedID 19124132
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Numerical Experiments with Shock-Turbulence Interaction
ASTRONOMICAL SOC PACIFIC. 2009: 31-41
View details for Web of Science ID 000267287200005
- LES of compressible turbulent flows: assessment of compact differencing with localized artificial diffusivity scheme 2009
- A low-order contrail model to use with global-scale climate models 2009
- Assessment of fast multipole method formulations for acoustic scattering 2009
- Large-eddy simulation of jet mixing in a supersonic turbulent crossflow 2009
- Noise predictions from cold high-speed turbulent jets using large-eddy simulation 2009
- Fast field solutions in acoustic analogy formulations 2009
- Direct numerical simulations of canonical shock/turbulence interaction 2009
- Numerical experiments with shock-turbulence interaction edited by Pogorelov, Nikolai, V., Audit, E., Colella, P. 2009
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Shock-turbulence Interaction: What we know and what we can learn from peta-scale Simulations
2009
View details for DOI 10.1088/1742-6596/180/1/012032
- Large eddy simulation of free-stream turbulence effects on heat-transfer to a high pressure turbine cascade 2009
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Shock-turbulence interaction: What we know and what we can learn from peta-scale simulations
IOP PUBLISHING LTD. 2009
View details for DOI 10.1088/1742-6596/180/1/012032
View details for Web of Science ID 000281436700033
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Low-frequency sound sources in high-speed turbulent jets
JOURNAL OF FLUID MECHANICS
2008; 617: 231-253
View details for DOI 10.1017/S0022112008004096
View details for Web of Science ID 000261707700011
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Localized artificial diffusivity scheme for discontinuity capturing on curvilinear meshes
JOURNAL OF COMPUTATIONAL PHYSICS
2008; 227 (22): 9498-9526
View details for DOI 10.1016/j.jcp.2008.06.034
View details for Web of Science ID 000260645700010
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Computational framework for coupling compressible and low Mach number codes
AIAA JOURNAL
2008; 46 (8): 1990-2001
View details for DOI 10.2514/1.32884
View details for Web of Science ID 000258281400010
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Evolution of isolated turbulent trailing vortices
PHYSICS OF FLUIDS
2008; 20 (3)
View details for DOI 10.1063/1.2840200
View details for Web of Science ID 000254537600024
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Current status of jet noise predictions using large-eddy simulation
AMER INST AERONAUT ASTRONAUT. 2008: 364-380
View details for DOI 10.2514/1.24475
View details for Web of Science ID 000252822800008
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NEAR FIELD OF FILM COOLING JET ISSUED INTO A FLAT PLATE BOUNDARY LAYER: LES STUDY
PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B
2008: 409-418
View details for Web of Science ID 000262638400037
- Sound generation due to transient motion of a bluff body: direct computation and acoustic analogy predictions 2008
- Simulation strategies for shock-turbulence interaction 2008
- Development of large eddy simulation for aero-thermal prediction in high-pressure turbine cascade 2008
- Mechanisms of jet mixing in a supersonic crossflow: a study using large-eddy simulation 2008
- Fast multipole boundary element method for sound scattering from aerodynamic bodies 2008
- Investigation of the role of instability waves in jet noise radiation 2008
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Toward petascale shock/turbulence computations
IOP PUBLISHING LTD. 2008
View details for DOI 10.1088/1742-6596/125/1/012045
View details for Web of Science ID 000260370700046
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Stagnation-point flow under free-stream turbulence
JOURNAL OF FLUID MECHANICS
2007; 590: 1-33
View details for DOI 10.1017/S0022112007007768
View details for Web of Science ID 000251286500001
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Sound generated by instability wave/shock-cell interaction in supersonic jets
JOURNAL OF FLUID MECHANICS
2007; 587: 173-215
View details for DOI 10.1017/S0022112007007306
View details for Web of Science ID 000250675300008
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Interaction of vortex wakes and buoyant jets: A study of two-dimensional dynamics
PHYSICS OF FLUIDS
2007; 19 (8)
View details for DOI 10.1063/1.2753515
View details for Web of Science ID 000249156500044
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An artificial nonlinear diffusivity method for supersonic reacting flows with shocks
JOURNAL OF COMPUTATIONAL PHYSICS
2007; 222 (1): 246-264
View details for DOI 10.1016/j.jcp.2006.07.020
View details for Web of Science ID 000244841300013
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Leading-edge effects in bypass transition
JOURNAL OF FLUID MECHANICS
2007; 572: 471-504
View details for DOI 10.1017/S0022112006001893
View details for Web of Science ID 000244434700022
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Computational issues and algorithm assessment for shock/turbulence interaction problems
IOP PUBLISHING LTD. 2007
View details for DOI 10.1088/1742-6596/78/1/012014
View details for Web of Science ID 000250667200014
- Computational issues and algorithm assessment for shock-turbulence interaction problems 2007
- Noise radiation predictions from jet instability waves using a hybrid nonlinear PSE-acoustic analogy 2007
- Identification of instability waves in high speed turbulent jets 2007
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Robustness of acoustic analogies for predicting mixing-layer noise
AIAA JOURNAL
2006; 44 (11): 2780-2786
View details for DOI 10.2514/1.22186
View details for Web of Science ID 000241851100041
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Computational acoustics in spherical geometry: Steps toward validating helioseismology
ASTROPHYSICAL JOURNAL
2006; 648 (2): 1268-1275
View details for Web of Science ID 000240403600047
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On the extension of the Boussinesq approximation for inertia dominated flows
PHYSICS OF FLUIDS
2006; 18 (6)
View details for DOI 10.1063/1.2206188
View details for Web of Science ID 000238731500034
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Computational prediction of flow-generated sound
ANNUAL REVIEW OF FLUID MECHANICS
2006; 38: 483-512
View details for Web of Science ID 000235373900018
- Investigating broadband shock-associated noise of axisymmetric jets using large-eddy simulation 2006
- Prediction of sound generated by a pitching airfoil: a comparison of RANS and LES 2006
- Far-field Jet Acoustics LES for Acoustics edited by Wagner, C., Hutt, T., Sagaut, P. Cambridge University Press.. 2006: 1
- On extension of the Boussinesq approximation for inertia dominated flows Phys. Fluids 2006; 18: 066601, (12 pages)
- Review of the current status of jet noise predictions using large-eddy simulation 2006
- Numerical investigations of a transverse jet in a supersonic crossflow using large-eddy simulation 2006
- Large-eddy simulation of film-cooling flow above a flat plate from inclined cylindrical holes 2006
- Large-eddy simulation of film-cooling flows in a model turbine blade leading edge 2006
- Large-eddy simulations of early stage contrails: effect of atmospheric properties 2006
- Sound generated by instability wave/shock-cell interaction in supersonic jets 2006
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LARGE EDDY SIMULATION OF FILM COOLING FLOW ABOVE A FLAT PLATE FROM INCLINED CYLINDRICAL HOLES
AMER SOC MECHANICAL ENGINEERS. 2006: 817-825
View details for Web of Science ID 000270164100096
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On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets (vol 17, pg 085103, 2005)
PHYSICS OF FLUIDS
2005; 17 (11)
View details for DOI 10.1063/1.2131828
View details for Web of Science ID 000233603000044
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Receptivity of the compressible mixing layer
JOURNAL OF FLUID MECHANICS
2005; 540: 301-335
View details for DOI 10.1017/S0022112005005884
View details for Web of Science ID 000232747000015
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On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets
PHYSICS OF FLUIDS
2005; 17 (8)
View details for DOI 10.1063/1.2001689
View details for Web of Science ID 000231392000028
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New answers on the interaction between polymers and vortices in turbulent flows
FLOW TURBULENCE AND COMBUSTION
2005; 74 (4): 311-329
View details for DOI 10.1004/s10494-005-9002-6
View details for Web of Science ID 000235281500002
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Convective and absolute electrokinetic instability with conductivity gradients
JOURNAL OF FLUID MECHANICS
2005; 524: 263-303
View details for DOI 10.1017/S0022112004002381
View details for Web of Science ID 000227786800013
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Direct numerical simulation of polymer-induced drag reduction in turbulent boundary layer flow
PHYSICS OF FLUIDS
2005; 17 (1)
View details for DOI 10.1063/1.1829751
View details for Web of Science ID 000226358000005
- High-speed jet aeroacoustics: a perspective from numerical simulations edited by Humphrey, J., Gatski, T. 2005
- Phased-array models of shock-cell noise sources 2005
- Towards large-eddy simulation of film-cooling flows in a model turbine blade leading edge 2005
- Sound generation by unsteady airfoil motions: a study using direct computation and acoustic analogy 2005
- Generation of low frequency sound in turbulent jets 2005
- Simulations of aircraft wake-exhaust mixing using LES: contrail formation in the near-field 2005
- Aeroacoustics of high-speed jets: a perspective from numerical simulations edited by Humphrey, J., Gatski, T. 2005
- Spatio-temporal multi-scale PSE for shear layer dynamics and acoustic radiation 2005
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Distortion of upstream disturbances in a Hiemenz boundary layer
JOURNAL OF FLUID MECHANICS
2004; 519: 201-232
View details for DOI 10.1017/s0022112004001247
View details for Web of Science ID 000225721500009
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On the computation of space-time correlations by large-eddy simulation
PHYSICS OF FLUIDS
2004; 16 (11): 3859-3867
View details for DOI 10.1063/1.1779251
View details for Web of Science ID 000224456800006
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Simple method for generating inflow turbulence
AIAA JOURNAL
2004; 42 (10): 2164-2166
View details for Web of Science ID 000224424200022
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On the coherent drag-reducing and turbulence-enhancing behaviour of polymers in wall flows
JOURNAL OF FLUID MECHANICS
2004; 514: 271-280
View details for DOI 10.1017/S0022112004000291
View details for Web of Science ID 000224223600011
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Computational aeroacoustics: progress on nonlinear problems of sound generation
PROGRESS IN AEROSPACE SCIENCES
2004; 40 (6): 345-416
View details for DOI 10.1016/j.paerosci.2004.09.001
View details for Web of Science ID 000225743000002
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Simulated polymer stretch in a turbulent flow using Brownian dynamics
JOURNAL OF FLUID MECHANICS
2004; 504: 61-71
View details for DOI 10.1017/S0022112004008250
View details for Web of Science ID 000221274000003
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Noise radiation from high-speed jets: Some insights from numerical simulations
SPRINGER. 2004: 415-430
View details for Web of Science ID 000243594100045
- Acoustic radiation from subsonic and supersonic mixing layers with nonlinear PSE 2004
- Computational Aeroacoustics: a review of numerical approaches and progress in nonlinear problems of sound generation Progress in Aerospace Sciences 2004; 6 (40): 345-416
- On sound generated by instability wave-shock cell interaction in supersonic jets 2004
- Jet noise prediction of cold and hot subsonic jets using large-eddy simulation 2004
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A robust high-order compact method for large eddy simulation
JOURNAL OF COMPUTATIONAL PHYSICS
2003; 191 (2): 392-419
View details for DOI 10.1016/S0021-9991(03)00322-X
View details for Web of Science ID 000186667400003
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Shock leakage through an unsteady vortex-laden mixing layer: application to jet screech
JOURNAL OF FLUID MECHANICS
2003; 490: 139-167
View details for DOI 10.1017/S0022112003005214
View details for Web of Science ID 000185536500007
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Direct numerical simulation of stagnation region flow and heat transfer with free-stream turbulence
PHYSICS OF FLUIDS
2003; 15 (6): 1462-1484
View details for DOI 10.1063/1.1565332
View details for Web of Science ID 000182795300012
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Green's functions for a source in a mixing layer: direct waves, refracted arrival waves and instability waves
JOURNAL OF FLUID MECHANICS
2003; 477: 89-128
View details for DOI 10.1017/S0022112002003087
View details for Web of Science ID 000182414800004
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Green's functions for a source in a boundary layer: direct waves, channelled waves and diffracted waves
JOURNAL OF FLUID MECHANICS
2003; 477: 129-173
View details for DOI 10.1017/S0022112002003099
View details for Web of Science ID 000182414800005
- Application of Adjoint Solutions to the Receptivity Problem in Compressible Mixing Layers 2003
- Simulation and analogies of stagnation point heat transfer under free-stream turbulence 2003
- The noise radiated by high-speed jets: some insights from numerical simulations 2003
- Sound Generation Mechanism of Shock-Associated Noise 2003
- A Statistical Subgrid Scale Noise Model: Formulation 2003
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A highly accurate technique for the treatment of flow equations at the polar axis in cylindrical coordinates using series expansions
JOURNAL OF COMPUTATIONAL PHYSICS
2002; 183 (1): 165-186
View details for DOI 10.1006/jcph.2002.7187
View details for Web of Science ID 000180053400006
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Refracted arrival waves in a zone of silence from a finite thickness mixing layer
JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA
2002; 111 (2): 716-728
Abstract
Refracted arrival waves which propagate in the zone of silence of a finite thickness mixing layer are analyzed using geometrical acoustics in two dimensions. Here, two simplifying assumptions are made: (i) the mean flow field is transversely sheared, and (ii) the mean velocity and temperature profiles approach the free-stream conditions exponentially. Under these assumptions, ray trajectories are analytically solved, and a formula for acoustic pressure amplitude in the far field is derived in the high-frequency limit. This formula is compared with the existing theory based on a vortex sheet corresponding to the low-frequency limit. The analysis covers the dependence on the Mach number as well as on the temperature ratio. The results show that both limits have some qualitative similarities, but the amplitude in the zone of silence at high frequencies is proportional to omega(-1/2), while that at low frequencies is proportional to omega(-3/2), omega being the angular frequency of the source.
View details for Web of Science ID 000173784900007
View details for PubMedID 11863174
- A numerical technique for trailing-edge acoustic scattering problems 2002
- A numerical study of broad-band shock noise 2002
- Numerical simulation of trailing edge receptivity 2002
- Spatial scale decomposition of shear layer turbulence and the sound sources associated with the missing scales in a large-eddy simulation 2002
- A numerical investigation of broad-band shock noise 2002
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Thermal perturbation of trailing vortices
GAUTHIER-VILLARS/EDITIONS ELSEVIER. 2001: 511-524
View details for Web of Science ID 000171230900005
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Vortex-wake pollution: A problem in fluid mechanics
SPRINGER-VERLAG BERLIN. 2001: 163-181
View details for Web of Science ID 000179942200009
- Computational Aeroacoustics 2001 Yearbook of Science and Technology Mc Graw Hill. 2001: 107-111
- Numerical study of leading edge heat transfer under free-stream turbulence 2001
- Direct numerical simulation of spatially developing, compressible, turbulent mixing layers 2001
- Computer Simulation and Prediction of Jet Noise High Speed Jet Flows edited by Raman, G., Mclaughlin, D., Morris, P. Taylor & Francis. 2001: 1
- Computational Aeroacoustics for Jet Noise Physics 2001
- Prediction of shock-cell structure using parabolized stability equations 2001
- Computational Aeroacoustics 2001 Yearbook of Science and Technology 2001: 107-111
- Large Eddy Simulation of a near sonic turbulent jet and its radiated noise 2001
- Shock leakage through an unsteady vortex-laden mixing layer: application to jet screech 2001
- Computational Aeroacoustics for Jet Noise Physics edited by Lumley, J., L. 2001
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Numerical simulation of a Mach 1.92 turbulent jet and its sound field
AMER INST AERONAUT ASTRONAUT. 2000: 2023-2031
View details for Web of Science ID 000165136400004
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Compressibility effects in a turbulent annular mixing layer. Part 2. Mixing of a passive scalar
JOURNAL OF FLUID MECHANICS
2000; 421: 269-292
View details for Web of Science ID 000165275100009
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Compressibility effects in a turbulent annular mixing layer. Part 1. Turbulence and growth rate
JOURNAL OF FLUID MECHANICS
2000; 421: 229-267
View details for Web of Science ID 000165275100008
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Influence of inflow disturbances on stagnation-region heat transfer
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME
2000; 122 (2): 258-265
View details for Web of Science ID 000168583600006
- Computational Aeroacoustics: Recent Progress and Current Challenges 2000
- A Numerical investigation of sound generation in supersonic jet screech 2000
- Computational Aeroacoustics: Recent Progress and Current Challenges 2000
- Direct numerical simulation of a low Reynolds number Mach 1.92 turbulent jet and its sound field AIAA Journal 2000; 38: 2023-2031
- Green’s functions in a boundary layer: low and high frequency asymptotes 2000
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Asymptotic growth of disturbances from spatially compact source in a skewed mixing layer
PHYSICS OF FLUIDS
1999; 11 (5): 1153-1160
View details for Web of Science ID 000079767300021
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Direct computation of the sound generated by vortex pairing in an axisymmetric jet
JOURNAL OF FLUID MECHANICS
1999; 383: 113-142
View details for Web of Science ID 000079765300005
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Method for accelerating the destruction of aircraft wake vortices
AMER INST AERONAUT ASTRONAUT. 1999: 398-404
View details for Web of Science ID 000079614200010
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Receptivity to surface roughness near a swept leading edge
JOURNAL OF FLUID MECHANICS
1999; 380: 141-168
View details for Web of Science ID 000079238100006
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Inviscid instability of compressible swirling mixing layers
PHYSICS OF FLUIDS
1999; 11 (2): 450-461
View details for Web of Science ID 000078167000021
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Direct numerical simulations of compressible turbulent flows: Fundamentals and applications
SPRINGER. 1999: 421-488
View details for Web of Science ID 000087037800007
- Acoustic Scattering from a Mixing Layer: Role of Instability Waves 1999
- A method for accelerating the destruction of aircraft-wake vortices Journal of Aircraft 1999; 36: 398-404
- Direct Numerical Simulation of Compressible Turbulent Flows: Fundamentals and Applications Turbulence and Combustion Modeling edited by Alfredsson, H., Johansson, A., Henningson, D. Kluwer Academic Publishing. 1999: 421-488
- Large-Eddy Simulation of a Mach 0.9 Turbulent Jet 1999
- Numerical Simulation of Shock-Vortex Interaction in Supersonic Jet Screech 1998
- Mechanism for Accelerating the Destruction of Aircraft Wake Vortices 1998
- Shock-vortex interactions in supersonic jet screech: an update 1998
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Direct computation of Mach wave radiation in an axisymmetric supersonic jet
AIAA JOURNAL
1997; 35 (10): 1574-1580
View details for Web of Science ID A1997XZ32000003
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Numerical method for incompressible vortical flows with two unbounded directions
JOURNAL OF COMPUTATIONAL PHYSICS
1997; 137 (1): 101-129
View details for Web of Science ID A1997YF66700004
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Interaction of isotropic turbulence with shock waves: Effect of shock strength
JOURNAL OF FLUID MECHANICS
1997; 340: 225-247
View details for Web of Science ID A1997XF40100009
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The influence of entropy fluctuations on the interaction of turbulence with a shock wave
JOURNAL OF FLUID MECHANICS
1997; 334: 353-379
View details for Web of Science ID A1997WR67900013
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Sound generation in a mixing layer
JOURNAL OF FLUID MECHANICS
1997; 330: 375-409
View details for Web of Science ID A1997WG78700016
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Flows with density variations and compressibility: Similarities and differences
SPRINGER. 1997: 279-301
View details for Web of Science ID A1997BJ82N00036
- Computational Aeroacoustics: A Review invited lecture at the 35th Aerospace Sciences Meeting and Exhibit, AIAA Paper 97-0018 1997
- Direct Simulation of a Supersonic Round Turbulent Shear Layer 1997
- Computational Aeroacoustics: A Review 1997
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Computation of quadrupole noise using acoustic analogy
AIAA JOURNAL
1996; 34 (11): 2247-2254
View details for Web of Science ID A1996VQ10800004
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Sound radiation during local laminar breakdown in a low-Mach-number boundary layer
JOURNAL OF FLUID MECHANICS
1996; 319: 197-218
View details for Web of Science ID A1996VD01300009
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Calculation of the radiated sound field using an open Kirchhoff surface
AIAA JOURNAL
1996; 34 (5): 909-916
View details for Web of Science ID A1996UH93500005
- Compressible and Hypersonic Flows Research Trends in Fluid Mechanics, Report by US National Committee for Theoretical and Applied Mechanics, published by American Institute of Physics 1996: 138-147
- Sound Radiation During Local Laminar Breakdown in a Low Mach Number Boundary Layer Journal of Fluid Mechanics 1996; 319: 197-218
- A Computational Approach to Swept Leading-Edge Receptivity 1996
- The Direct Computation of Mach Wave Radiation in an Axisymmetric Supersonic Jet 1996
- Direct Numerical Simulation of the breakdown of Aircraft Wake Vortices 1996
- Compressible and Hypersonic Flows Research Trends in Fluid Mechanics, Report by US National Committee for Theoretical and Applied Mechanics American Institute of Physics. 1996: 138-147
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THE INTERACTION OF AN ISOTROPIC FIELD OF ACOUSTIC-WAVES WITH A SHOCK-WAVE
JOURNAL OF FLUID MECHANICS
1995; 300: 383-407
View details for Web of Science ID A1995TD01400016
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DIRECT COMPUTATION OF THE SOUND FROM A COMPRESSIBLE CO-ROTATING VORTEX PAIR
JOURNAL OF FLUID MECHANICS
1995; 285: 181-202
View details for Web of Science ID A1995QK09100008
- Direct Computation of the Sound Generated by Vortex Pairing in an Axisymmetric Jet 1995
- The Sound Generated by a Two-Dimensional Shear Layer: A Comparison of Direct Computations and Acoustic Analogies 1995
- Calculation of the Radiated Sound Field Using an Open Kirchhoff Surface 1995
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THE SCATTERING OF SOUND-WAVES BY A VORTEX - NUMERICAL SIMULATIONS AND ANALYTICAL SOLUTIONS
JOURNAL OF FLUID MECHANICS
1994; 260: 271-298
View details for Web of Science ID A1994MZ16300011
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ON THE DENSITY RATIO EFFECT ON THE GROWTH-RATE OF A COMPRESSIBLE MIXING LAYER
AMER INST PHYSICS. 1994: 1073-1075
View details for Web of Science ID A1994NA73900033
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THE RESPONSE OF ANISOTROPIC TURBULENCE TO RAPID HOMOGENEOUS ONE-DIMENSIONAL COMPRESSION
AMER INST PHYSICS. 1994: 1052-1062
View details for Web of Science ID A1994NA73900031
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COMPRESSIBILITY EFFECTS ON TURBULENCE
ANNUAL REVIEW OF FLUID MECHANICS
1994; 26: 211-254
View details for Web of Science ID A1994MT01700009
- Interaction of Isotropic Turbulence With a Strong Shock Wave 1994
- A Note on the Density Ratio Effect on the Growth Rate of a Compressible Mixing Layer The Physics of Fluids A 1994; 6: 1073-1075
- Vortex Breakdown in Skewed Compressible Mixing Layers 1994
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THE EVOLUTION OF A PLANE MIXING LAYER WITH SPANWISE NONUNIFORM FORCING
PHYSICS OF FLUIDS
1994; 6 (1): 381-396
View details for Web of Science ID A1994NA73700038
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BOUNDARY-CONDITIONS FOR DIRECT COMPUTATION OF AERODYNAMIC SOUND GENERATION
AIAA JOURNAL
1993; 31 (9): 1574-1582
View details for Web of Science ID A1993LU62500005
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DIRECT NUMERICAL-SIMULATION OF ISOTROPIC TURBULENCE INTERACTING WITH A WEAK SHOCK-WAVE
JOURNAL OF FLUID MECHANICS
1993; 251: 533-562
View details for Web of Science ID A1993LK38200021
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VORTEX-INDUCED DISTURBANCE FIELD IN A COMPRESSIBLE SHEAR-LAYER
PHYSICS OF FLUIDS A-FLUID DYNAMICS
1993; 5 (6): 1412-1419
View details for Web of Science ID A1993LE35600015
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INVISCID INSTABILITY OF A SKEWED COMPRESSIBLE MIXING LAYER
JOURNAL OF FLUID MECHANICS
1993; 249: 441-463
View details for Web of Science ID A1993KZ44700020
- Direct Simulation of Shock-Turbulence Interaction Journal of Fluid Mechanics, 1993: corrigendum in Journal of Fluid Mechanics 1993, 1994; 251, 264: 373-374, 533-562
- A Comparative Study of Turbulence Decay Using Navier-Stokes and a Discrete Particle Simulation 1993
- Shock Turbulence Interaction in the Presence of Mean Shear: An Application of Rapid Distortion Theory 1993
- Spatial Growth of Disturbances in a Skewed Compressible Mixing Layer 1993
- Matching of Near/Far-field Equation Sets for Direct Computations of Aerodynamic Sound 1993
- Direct Computation of the Sound Generated by a Two-Dimensional Shear Layer 1993
- Boundary Conditions for Direct Computation of Aerodynamic Sound Generation AIAA Journal 1993; 31: 1574-1582
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SHOCK-JUMP RELATIONS IN A TURBULENT-FLOW
PHYSICS OF FLUIDS A-FLUID DYNAMICS
1992; 4 (12): 2900-2905
View details for Web of Science ID A1992KA35700028
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COMPACT FINITE-DIFFERENCE SCHEMES WITH SPECTRAL-LIKE RESOLUTION
JOURNAL OF COMPUTATIONAL PHYSICS
1992; 103 (1): 16-42
View details for Web of Science ID A1992JV66900002
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VORTICITY FORM OF TURBULENCE TRANSPORT-EQUATIONS
PHYSICS OF FLUIDS A-FLUID DYNAMICS
1992; 4 (8): 1767-1772
View details for Web of Science ID A1992JE92300020
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BOUNDARY-CONDITIONS FOR DIRECT SIMULATIONS OF COMPRESSIBLE VISCOUS FLOWS
JOURNAL OF COMPUTATIONAL PHYSICS
1992; 101 (1): 104-129
View details for Web of Science ID A1992JF12700009
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SIMULATION OF SPATIALLY EVOLVING TURBULENCE AND THE APPLICABILITY OF TAYLOR HYPOTHESIS IN COMPRESSIBLE FLOW
PHYSICS OF FLUIDS A-FLUID DYNAMICS
1992; 4 (7): 1521-1530
View details for Web of Science ID A1992HZ84200018
- Boundary Conditions for Direct Computations of Aerodynamic Sound Generation 1992
- Direct Computation of the Sound From a Compressible Co-rotating Vortex Pair 1992
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THE FREE COMPRESSIBLE VISCOUS VORTEX
JOURNAL OF FLUID MECHANICS
1991; 230: 45-73
View details for Web of Science ID A1991GH08800002
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EDDY SHOCKLETS IN DECAYING COMPRESSIBLE TURBULENCE
PHYSICS OF FLUIDS A-FLUID DYNAMICS
1991; 3 (4): 657-664
View details for Web of Science ID A1991FE06000018
- Motion of Particles With Inertia in a Compressible Free Shear Layer The Physics of Fluids A 1991; 3: 1915-1923
- Scattering of Sound Waves by a Compressible Vortex 1991
- Particle Laden Compressible Shear Layers 1990
- Nonlinear Dynamics in Langmuir Circulations and in Thermosolutal Convection Journal of Fluid Mechanics 1989; 198: 471-511
- Direct Numerical Simulation of Compressible Free Shear Flows 1989
- A Consistency Condition for Reynolds Stress Closures Physics of Fluids 1985; 28: 64-68
- The Influence of the Horizontal Component of the Earth’s Angular Velocity on the Instability of the Ekman Layer Journal of Fluid Mechanics 1985; 150: 41-87