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.

Honors & Awards


  • AIAA Wind Energy Conference Best Paper Award with Aditya Ghate, Niranjan Ghaisas and Aaron Towne, American Institute of Aeronautics and Astronautics (2019)
  • Distinguished Alumnus Award, IIT Kanpur, India (2017)
  • AIAA Aeroacoustics Award, American Institute of Aeronautics & Astronautics (2016)
  • AIAA Best Paper Award with David Dawson, AIAA Fluid Dynamics Technical Committee (2015)
  • Associate Fellow AIAA, American Institute of Aeronautics and Astronautics (2015)
  • AIAA Best Paper Award with Britton Olson, AIAA Fluid Dynamics Technical Committee (2012)
  • AIAA Best Student Paper Award with William Wolf, AIAA/CEAS Aeroacoustics Conference (2011)
  • Stanford Asian American Faculty Award, Stanford Asian American Faculty (2004)
  • Fellow American Physical Society, American Physical Society (2001)
  • RT Knapp Award with Ted Manning, ASME Fluids Engineering Division (1999)
  • Presidential Young Investigator Award, National Science Foundation (1991)
  • F N Frenkiel Award, American Physical Society, Division of Fluid Dynamics (1986)

Boards, Advisory Committees, Professional Organizations


  • Associate Editor, Journal of Fluid Mechanics (1994 - 2004)
  • Associate Editor, Physical Review Fluids - American Physical Society (2021 - Present)

Professional Education


  • PhD, Cornell, Mechanical Engineering (1985)

2023-24 Courses


Stanford Advisees


All Publications


  • Analysis of second moments and their budgets for Richtmyer-Meshkov instability and variable-density turbulence induced by reshock PHYSICAL REVIEW FLUIDS Wong, M., Baltzer, J. R., Livescu, D., Lele, S. K. 2022; 7 (4)
  • Optimal closed-loop wake steering - Part 2: Diurnal cycle atmospheric boundary layer conditions WIND ENERGY SCIENCE Howland, M. F., Ghate, A. S., Quesada, J., Martinez, J., Zhong, W., Larranaga, F., Lele, S. K., Dabiri, J. O. 2022; 7 (1): 345-365
  • Subgrid-scale pressure field of scale-enriched large eddy simulations using Gabor modes PHYSICAL REVIEW FLUIDS Hass, R. D., Ghate, A. S., Lele, S. K. 2021; 6 (12)
  • Settling of two-way momentum and energy coupled particles subject to Boussinesq and non-Boussinesq heating THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS Horwitz, J. K., Ganguli, S., Lele, S. K., Mani, A. 2021
  • Homogenized Flux-Body Force Treatment of Compressible Viscous Porous Wall Boundary Conditions AIAA JOURNAL Huang, D. Z., Wong, M., Lele, S. K., Farhat, C. 2021; 59 (6): 2045-2059

    View details for DOI 10.2514/1.J059945

    View details for Web of Science ID 000658581200012

  • Optimal closed-loop wake steering - Part 1: Conventionally neutral atmospheric boundary layer conditions WIND ENERGY SCIENCE Howland, M. F., Ghate, A. S., Lele, S. K., Dabiri, J. O. 2020; 5 (4): 1315–38
  • Wind Turbine Performance in Very Large Wind Farms: Betz Analysis Revisited ENERGIES West, J. R., Lele, S. K. 2020; 13 (5)

    View details for DOI 10.3390/en13051078

    View details for Web of Science ID 000524318700065

  • Effect of tip spacing, thrust coefficient and turbine spacing in multi-rotor wind turbines and farms WIND ENERGY SCIENCE Ghaisas, N. S., Ghate, A. S., Lele, S. K. 2020; 5 (1): 51–72
  • Modelling of jet noise: a perspective from large-eddy simulations. Philosophical transactions. Series A, Mathematical, physical, and engineering sciences Bres, G. A., Lele, S. K. 2019; 377 (2159): 20190081

    Abstract

    In the last decade, many research groups have reported predictions of jet noise using high-fidelity large-eddy simulations (LES) of the turbulent jet flow and these methods are beginning to be used more broadly. A brief overview of the publications since the review by Bodony & Lele (2008, AIAA J. 56, 346-380) is undertaken to assess the progress and overall contributions of LES towards a better understanding of jet noise. In particular, we stress the meshing, numerical and modelling advances which enable detailed geometric representation of nozzle shape variations intended to impact the noise radiation, and sufficiently accurate capturing of the turbulent boundary layer at the nozzle exit. Examples of how LES is currently being used to complement experiments for challenging conditions (such as highly heated pressure-mismatched jets with afterburners) and guide jet modelling efforts are highlighted. Some of the physical insights gained from these numerical studies are discussed, in particular on crackle, screech and shock-associated noise, impingement tones, acoustic analogy models, wavepackets dynamics and resonant acoustic waves within the jet core. We close with some perspectives on the remaining challenges and upcoming opportunities for future applications. This article is part of the theme issue 'Frontiers of aeroacoustics research: theory, computation and experiment'.

    View details for DOI 10.1098/rsta.2019.0081

    View details for PubMedID 31607250

  • A high-order weighted compact high resolution scheme with boundary closures for compressible turbulent flows with shocks JOURNAL OF COMPUTATIONAL PHYSICS Subramaniam, A., Wong, M., Lele, S. K. 2019; 397
  • High-resolution Navier-Stokes simulations of Richtmyer-Meshkov instability with reshock PHYSICAL REVIEW FLUIDS Wong, M., Livescu, D., Lele, S. K. 2019; 4 (10)
  • Low Mach, compressibility, and finite size effects of localized uniform heat sources in a gas THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS Ganguli, S., Lele, S. K. 2019; 33 (3-4): 341–58
  • Wind farm power optimization through wake steering. Proceedings of the National Academy of Sciences of the United States of America Howland, M. F., Lele, S. K., Dabiri, J. O. 2019

    Abstract

    Global power production increasingly relies on wind farms to supply low-carbon energy. The recent Intergovernmental Panel on Climate Change (IPCC) Special Report predicted that renewable energy production must leap from [Formula: see text] of the global energy mix in 2018 to [Formula: see text] by 2050 to keep global temperatures from rising 1.5°C above preindustrial levels. This increase requires reliable, low-cost energy production. However, wind turbines are often placed in close proximity within wind farms due to land and transmission line constraints, which results in wind farm efficiency degradation of up to [Formula: see text] for wind directions aligned with columns of turbines. To increase wind farm power production, we developed a wake steering control scheme. This approach maximizes the power of a wind farm through yaw misalignment that deflects wakes away from downstream turbines. Optimization was performed with site-specific analytic gradient ascent relying on historical operational data. The protocol was tested in an operational wind farm in Alberta, Canada, resulting in statistically significant ([Formula: see text]) power increases of 7-[Formula: see text] for wind speeds near the site average and wind directions which occur during less than [Formula: see text] of nocturnal operation and 28-[Formula: see text] for low wind speeds in the same wind directions. Wake steering also decreased the variability in the power production of the wind farm by up to [Formula: see text] Although the resulting gains in annual energy production were insignificant at this farm, these statistically significant wake steering results demonstrate the potential to increase the efficiency and predictability of power production through the reduction of wake losses.

    View details for DOI 10.1073/pnas.1903680116

    View details for PubMedID 31262816

  • Drag of a heated sphere at low Reynolds numbers in the absence of buoyancy JOURNAL OF FLUID MECHANICS Ganguli, S., Lele, S. K. 2019; 869: 264–91
  • Modal analysis of the laminar boundary layer instability and tonal noise of an airfoil at Reynolds number 150,000 INTERNATIONAL JOURNAL OF AEROACOUSTICS Sanjose, M., Towne, A., Jaiswal, P., Moreau, S., Lele, S., Mann, A. 2019; 18 (2-3): 317–50
  • A unified high-order Eulerian method for continuum simulations of fluid flow and of elastic-plastic deformations in solids JOURNAL OF COMPUTATIONAL PHYSICS Ghaisas, N. S., Subramaniam, A., Lele, S. K. 2018; 371: 452–82
  • Importance of the nozzle-exit boundary-layer state in subsonic turbulent jets JOURNAL OF FLUID MECHANICS Bres, G. A., Jordan, P., Jaunet, V., Le Rallic, M., Cavalieri, A. G., Towne, A., Lele, S. K., Colonius, T., Schmidt, O. T. 2018; 851: 83–124
  • High-Order Eulerian Simulations of Multimaterial Elastic-Plastic Flow JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME Subramaniam, A., Ghaisas, N. S., Lele, S. K. 2018; 140 (5)

    View details for DOI 10.1115/1.4038399

    View details for Web of Science ID 000427848100005

  • Influence of the horizontal component of Earth's rotation on wind turbine wakes Howland, M. F., Ghate, A. S., Lele, S. K., IOP IOP PUBLISHING LTD. 2018
  • Large-eddy simulation study of multi-rotor wind turbines Ghaisas, N. S., Ghate, A. S., Lele, S. K., IOP IOP PUBLISHING LTD. 2018
  • Localized artificial diffusivity scheme for deflagrations and detonation waves COMPUTERS & FLUIDS Lee, C., Lele, S. K. 2017; 159: 33–52
  • High-order localized dissipation weighted compact nonlinear scheme for shock- and interface-capturing in compressible flows JOURNAL OF COMPUTATIONAL PHYSICS Wong, M. L., Lele, S. K. 2017; 339: 179-209
  • Unstructured Large-Eddy Simulations of Supersonic Jets AIAA JOURNAL Bres, G. A., Ham, F. E., Nichols, J. W., Lele, S. K. 2017; 55 (4): 1164-1184

    View details for DOI 10.2514/1.J055084

    View details for Web of Science ID 000400284700007

  • Instability waves in high-speed jets: near-and far-field DNS/LES data analysis INTERNATIONAL JOURNAL OF AEROACOUSTICS Ryu, J., Lele, S. K. 2015; 14 (3-4): 643-673
  • Stabilization of a hypersonic boundary layer using a felt-metal porous coating JOURNAL OF FLUID MECHANICS Tritarelli, R. C., Lele, S. K., Fedorov, A. 2015; 769: 729-739
  • Linear and nonlinear modelling of a theoretical travelling-wave thermoacoustic heat engine JOURNAL OF FLUID MECHANICS Scalo, C., Lele, S. K., Hesselink, L. 2015; 766
  • Compressible turbulent channel flow with impedance boundary conditions PHYSICS OF FLUIDS Scalo, C., Bodart, J., Lele, S. K. 2015; 27 (3)

    View details for DOI 10.1063/1.4914099

    View details for Web of Science ID 000352309400046

  • Study of supertonic wave components in high-speed turbulent jets using an LES database JOURNAL OF SOUND AND VIBRATION Ryu, J., Lele, S. K., Viswanathan, K. 2014; 333 (25): 6900-6923
  • Parameterization of Boundary-Layer Transition Induced by Isolated Roughness Elements AIAA JOURNAL Bernardini, M., Pirozzoli, S., Orlandi, P., Lele, S. K. 2014; 52 (10): 2261-2269

    View details for DOI 10.2514/1.J052842

    View details for Web of Science ID 000342759200013

  • On the Richtmyer-Meshkov instability evolving from a deterministic multimode planar interface JOURNAL OF FLUID MECHANICS Tritschler, V. K., Olson, B. J., Lele, S. K., Hickel, S., Hu, X. Y., Adams, N. A. 2014; 755
  • A second golden age of aeroacoustics? PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES Lele, S. K., Nichols, J. W. 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

  • Large-Eddy Simulations of a Normal Shock Train in a Constant-Area Isolator AIAA JOURNAL Morgan, B., Duraisamy, K., Lele, S. K. 2014; 52 (3): 539-558

    View details for DOI 10.2514/1.J052348

    View details for Web of Science ID 000337796100007

  • Effect of adverse pressure gradient on high speed boundary layer transition PHYSICS OF FLUIDS Franko, K. J., Lele, S. 2014; 26 (2)

    View details for DOI 10.1063/1.4864337

    View details for Web of Science ID 000332322000025

  • Numerical investigation of turbulence in reshocked Richtmyer-Meshkov unstable curtain of dense gas SHOCK WAVES Shankar, S. K., Lele, S. K. 2014; 24 (1): 79-95
  • Effects of mean flow convection, quadrupole sources and vortex shedding on airfoil overall sound pressure level JOURNAL OF SOUND AND VIBRATION Wolf, W. R., Azevedo, J. L., Lele, S. K. 2013; 332 (26): 6905-6912
  • Effects of plume-scale versus grid-scale treatment of aircraft exhaust photochemistry GEOPHYSICAL RESEARCH LETTERS Cameron, M. A., Jacobson, M. Z., Naiman, A. D., Lele, S. K. 2013; 40 (21): 5815-5820
  • Fast acoustic scattering predictions with non-uniform potential flow effects JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING Wolf, W. R., Lele, S. K. 2013; 35 (4): 407-418
  • A mechanism for unsteady separation in over-expanded nozzle flow PHYSICS OF FLUIDS Olson, B. J., Lele, S. K. 2013; 25 (11)

    View details for DOI 10.1063/1.4819349

    View details for Web of Science ID 000329184100010

  • Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers JOURNAL OF FLUID MECHANICS Franko, K. J., Lele, S. K. 2013; 730: 491-532
  • Flow physics and RANS modelling of oblique shock/turbulent boundary layer interaction JOURNAL OF FLUID MECHANICS Morgan, B., Duraisamy, K., Nguyen, N., Kawai, S., Lele, S. K. 2013; 729: 231-284
  • Directional artificial fluid properties for compressible large-eddy simulation JOURNAL OF COMPUTATIONAL PHYSICS Olson, B. J., Lele, S. K. 2013; 246: 207-220
  • Turbulent kinetic energy spectra of solar convection from New Solar Telescope observations and realistic magnetohydrodynamic simulations PHYSICA SCRIPTA Kitiashvili, I. N., Abramenko, V. I., Goode, P. R., Kosovichev, A. G., Lele, S. K., Mansour, N. N., Wray, A. A., Yurchyshyn, V. B. 2013; T155
  • UBIQUITOUS SOLAR ERUPTIONS DRIVEN BY MAGNETIZED VORTEX TUBES ASTROPHYSICAL JOURNAL Kitiashvili, I. N., Kosovichev, A. G., Lele, S. K., Mansour, N. N., Wray, A. A. 2013; 770 (1)
  • Crackle Noise in Heated Supersonic Jets JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME Nichols, J. W., Lele, S. K., Ham, F. E., Martens, S., Spyropoulos, J. T. 2013; 135 (5)

    View details for DOI 10.1115/1.4007867

    View details for Web of Science ID 000326154200002

  • Reynolds- and Mach-number effects in canonical shock-turbulence interaction JOURNAL OF FLUID MECHANICS Larsson, J., Bermejo-Moreno, I., Lele, S. K. 2013; 717: 293-321
  • On the use of the Ffowcs Williams-Hawkings equation to predict far-field jet noise from large-eddy simulations INTERNATIONAL JOURNAL OF AEROACOUSTICS Mendez, S., Shoeybi, M., Lele, S. K., Moin, P. 2013; 12 (1-2): 1-20
  • 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 Jacobson, M. Z., Wilkerson, J. T., Naiman, A. D., Lele, S. K. 2013; 165: 369-382

    View details for DOI 10.1039/c3fd00034f

    View details for Web of Science ID 000329068600019

  • 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. Jacobson, M., Z., Wilkerson, J., T., Naiman, A., D., Lele, S., K. 2013

    View details for DOI 10.1039/C3FD00034F

  • Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers J. Fluid Mech. Franko, K., Lele, S., K. 2013; 730: 491-532
  • Towards full-scale numerical simulations of travelling-wave thermoacoustic Stirling engines Scalo, C., Lin, J., Lele, S., K., Hesselink, L. 2013
  • Flow physics and RANS modeling of oblique shock/turbulent boundary layer interaction J. Fluid Mech. Morgan, B., Duraisamy, K., Nguyen, N., Kawai, S., Lele, S., K. 2013; 729: 231-284
  • Towards full-scale numerical simulations of travelling-wave thermoacoustic Stirling engines Scalo, C., Lin, J., Lele, S., K., Hesselink, L. 2013
  • Assessment of wall-modeled large-eddy simulation for supersonic compression ramp flows Dawson, D., M., Lele, S., K., Bodart, J. 2013
  • A probabilistic ice habit model for LES of contrails Inamdar, A., R., Lele, S., K., Jacobson, M., Z. 2013
  • Simulations of a normal shock train in a constant area duct using wall-modeled LES Vane, Z., P., Lele, S., K. 2013
  • A mechanism for unsteady separation in over-expanded nozzle flow Phys. Fluids. Olson, B., J., Lele, S., K. 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. Wolf, W., R., Azevedo, J., L. F., Lele, S., K. 2013
  • Directional artificial fluid properties for compressible large-eddy simulations J. Comput. Phys. Olson, B., J., Lele, S., K. 2013; 246: 207-220
  • The source of crackle noise in heated supersonic jets Nichols, J., W., Lele, S., K., Spyropoulos, J., T. 2013
  • Nozzle wall modeling in unstructured large-eddy simulations for hot supersonic jet predictions Bres, G., A., Ham, F., Nichols, J., W., Lele, S., K. 2013
  • Ovarian Cancer, Version 3.2012 Featured Updates to the NCCN Guidelines JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK Morgan, R. J., Alvarez, R. D., Armstrong, D. K., Burger, R. A., Castells, M., Chen, L., Copeland, L., Crispens, M. A., Gershenson, D., Gray, H., Hakam, A., Havrilesky, L. J., Johnston, C., Lele, S., Martin, L., Matulonis, U. A., O'Malley, D. M., Penson, R. T., Remmenga, S. W., Sabbatini, P., Santoso, J. T., Schilder, R. J., Schink, J., Teng, N., Werner, T. L., Hughes, M., Dwyer, M. A. 2012; 10 (11): 1339-1349

    Abstract

    These NCCN Guidelines Insights focus on the major updates for the 2012 NCCN Clinical Practice Guidelines in Oncology (NCCN Guidelines) for Ovarian Cancer by describing how and why the new recommendations were made. The 6 update topics were selected based on recent important updates in the guidelines and on debate among panel members about recent clinical trials, and include: 1) screening, 2) diagnostic tests for assessing pelvic masses, 3) primary treatment using neoadjuvant chemotherapy, 4) primary adjuvant treatment using bevacizumab in combination with chemotherapy, 5) therapy for recurrent disease, and 6) management of drug/hypersensitivity reactions. These NCCN Guidelines Insights also discuss why some recommendations were not made (eg, panel members did not feel the new data warranted changing the guideline). See "Updates" in the NCCN Guidelines for Ovarian Cancer for a complete list of all the recent revisions.

    View details for Web of Science ID 000310822900005

  • Trailing-Edge Noise Predictions Using Compressible Large-Eddy Simulation and Acoustic Analogy AIAA JOURNAL Wolf, W. R., Lele, S. K. 2012; 50 (11): 2423-2434

    View details for DOI 10.2514/1.J051638

    View details for Web of Science ID 000310559000011

  • Convective effects and the role of quadrupole sources for aerofoil aeroacoustics JOURNAL OF FLUID MECHANICS Wolf, W. R., Azevedo, J. L., Lele, S. K. 2012; 708: 502-538
  • Interaction of a converging spherical shock wave with isotropic turbulence PHYSICS OF FLUIDS Bhagatwala, A., Lele, S. K. 2012; 24 (8)

    View details for DOI 10.1063/1.4737892

    View details for Web of Science ID 000308417000035

  • Vortex tubes of turbulent solar convection PHYSICA SCRIPTA Kitiashvili, I. N., Kosovichev, A. G., Mansour, N. N., Lele, S. K., Wray, A. A. 2012; 86 (1)
  • Large-Eddy Simulations of Perfectly Expanded Supersonic Jets Using an Unstructured Solver 48th AIAA Aerospace Sciences Meeting Mendez, S., Shoeybi, M., Sharma, A., Ham, F. E., Lele, S. K., Moin, P. AMER INST AERONAUTICS ASTRONAUTICS. 2012: 1103–18

    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 Lee, J., Lele, S., K. 2012
  • Effects of Mean Flow Convection and Quadrupole Sources on Airfoil Trailing Edge Noise Wolf, W., Azevedo, J. L., Lele, S. 2012
  • Interaction of converging spherical shock wave with isotropic turbulence Physics of Fluids Bhagatwala, A., Lele, S., K. 2012; 24 (8): 21

    View details for DOI 10.1063/1.4737892

  • Large-eddy simulation for supersonic rectangular jet noise prediction: effects of chevrons Nichols, J., Lele, S., Moin, P., Ham, F., Brès, G., Bridges, J. 2012
  • Investigation of Noise Generated by a DU96 Airfoil Wolf, W., Azevedo, J. L., Lele, S. 2012
  • Large-eddy and RANS simulations of normal shock train in a constant area isolator Morgan, B., Duraisamy, K., Lele, S., K. 2012
  • Large-eddy simulation of perfectly expanded supersonic jets using unstructured solver AIAA J. Mendez, S., Shoeybi, M., Sharma, A., Ham, F., E., Lele, S., K., Moin, P. 2012; 50: 1103-1118
  • Low Frequency Unsteadiness in Nozzle Flow Separation Olson, B., Lele, S. 2012
  • Aeroacoustics of a supersonic rectangular jet: experiments and LES predictions Nichols, J., W., Ham, F., Lele, S., K., Bridges, J., E. 2012
  • Crackle noise in heated supersonic jets Nichols, J., W., Lele, S., K., Ham, F., E., Marten, S., Spyropoulos, J., T. 2012
  • Crackle noise in heated supersonic jets J. Eng. Gas Turbines & Power, GTP-12-1155. Nichols, J., W., Lele, S., K., Ham, F., E., Martens, S., Spyropoulos, J., T. 2012
  • Unstructured Large Eddy Simulation of a Hot Supersonic Over-Expanded Jet with Chevrons Brès, G., Nichols, J., Lele, S., Ham, F., Schlinker, R., Reba, R. 2012
  • Directional artificial bulk viscosity for shock capturing on high aspect ratio grids Comput. Science & Discovery Olson, B., J., Lele, S., K. 2012; 5: 14008
  • Effects of heating on noise radiation from turbulent mixing layers with initially laminar and turbulent boundary layers Sharma, A., Lele, S., K. 2012
  • Wideband fast multipole boundary element method: Application to acoustic scattering from aerodynamic bodies INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS Wolf, W. R., Lele, S. K. 2011; 67 (12): 2108-2129

    View details for DOI 10.1002/fld.2486

    View details for Web of Science ID 000297736100020

  • Non-normal global modes of high-speed jets INTERNATIONAL JOURNAL OF SPRAY AND COMBUSTION DYNAMICS Nichols, J. W., Lele, S. K. 2011; 3 (4): 285-301
  • Large eddy simulations of contrail development: Sensitivity to initial and ambient conditions over first twenty minutes JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES Naiman, A. D., Lele, S. K., Jacobson, M. Z. 2011; 116
  • Nonlinear effects in the combined Rayleigh-Taylor/Kelvin-Helmholtz instability PHYSICS OF FLUIDS Olson, B. J., Larsson, J., Lele, S. K., Cook, A. W. 2011; 23 (11)

    View details for DOI 10.1063/1.3660723

    View details for Web of Science ID 000297939200026

  • Vertical mixing of commercial aviation emissions from cruise altitude to the surface JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES Whitt, D. B., Jacobson, M. Z., Wilkerson, J. T., Naiman, A. D., Lele, S. K. 2011; 116
  • Aeroacoustic Integrals Accelerated by Fast Multipole Method AIAA JOURNAL Wolf, W. R., Lele, S. K. 2011; 49 (7): 1466-1477

    View details for DOI 10.2514/1.J050861

    View details for Web of Science ID 000293113500014

  • 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 Jacobson, M. Z., Wilkerson, J. T., Naiman, A. D., Lele, S. K. 2011; 230 (12): 5115-5132
  • Sound generation due to unsteady motion of a cylinder PHYSICS OF FLUIDS Sharma, A., Lele, S. K. 2011; 23 (4)

    View details for DOI 10.1063/1.3579489

    View details for Web of Science ID 000290050000038

  • Improving Low-Frequency Characteristics of Recycling/Rescaling Inflow Turbulence Generation AIAA JOURNAL Morgan, B., Larsson, J., Kawai, S., Lele, S. K. 2011; 49 (3): 582-597

    View details for DOI 10.2514/1.J050705

    View details for Web of Science ID 000288059200012

  • Interaction of a Taylor blast wave with isotropic turbulence PHYSICS OF FLUIDS Bhagatwala, A., Lele, S. K. 2011; 23 (3)

    View details for DOI 10.1063/1.3560384

    View details for Web of Science ID 000289153000028

  • Two-dimensional viscous flow simulation of a shock accelerated heavy gas cylinder PHYSICS OF FLUIDS Shankar, S. K., Kawai, S., Lele, S. K. 2011; 23 (2)

    View details for DOI 10.1063/1.3553282

    View details for Web of Science ID 000287812800022

  • Global modes and transient response of a cold supersonic jet JOURNAL OF FLUID MECHANICS Nichols, J. W., Lele, S. K. 2011; 669: 225-241
  • Epithelial Ovarian Cancer JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK Morgan, R. J., Alvarez, R. D., Armstrong, D. K., Boston, B., Burger, R. A., Chen, L., Copeland, L., Crispens, M. A., Gershenson, D., Gray, H. J., Grigsby, P. W., Hakam, A., Havrilesky, L. J., Johnston, C., Lele, S., Matulonis, U. A., O'Malley, D. M., Penson, R. T., Remmenga, S. W., Sabbatini, P., Schilder, R. J., Schink, J. C., Teng, N., Werner, T. L. 2011; 9 (1): 82-113

    View details for Web of Science ID 000287217200008

    View details for PubMedID 21233246

  • Effects of heating on noise radiation from a two-dimensional mixing layer: direct computation and acoustic analogy predictions Sharma, A., Lele, S., K. 2011
  • Large eddy simulation of an over-expanded planar nozzle Olson, B., Lele, S., K. 2011
  • High-fidelity large-eddy simulation for supersonic rectangular jet noise prediction Nichols, J., Ham, F., Lele, S., K. 2011
  • Large eddy simulation of a Mach 2.9 turbulent boundary layer over a 24 deg compression ramp Dawson, D., Kawai, S., Lele, S., K. 2011
  • Analysis and correction of errors generated by slowly moving shocks Johnsen, E., Lele, S., K. 2011
  • Large eddy simulation of persistent aircraft contrails Naiman, A., D., Lele, S., K., Jacobson, M., Z 2011
  • Unstructured large-eddy simulation for prediction of noise issued from turbulent jets in various configurations Khalighi, Y., Nichols, J., Lele, S., K., Ham, F., Moin, P. 2011
  • Direct simulation of transition and heat-transfer overshoot in a Mach 6 flat plate boundary layer Bhaskaran, R., Franko, K., Lele, S., K. 2011
  • LES of tripped super-critical cylinder flow: towards tandem cylinder noise prediction Yu, C., Wolf, W., Lele, S., K. 2011
  • Trailing edge noise predictions using compressible LES and acoustic analogy Wolf, W., Lele, S., K. 2011
  • A parametric investigation of oblique shockwave/turbulent boundary layer interaction using LES Morgan, B., Kawai, S., Lele, S., K. 2011
  • Large-eddy simulation of supersonic, turbulent mixing layers downstream of a splitter plate Sharma, A., Lele, S., K. 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. Jacobson, M., Z., Wilkerson, J., T., Naiman, A., D., Lele, S., K. 2011; 230 (12): 5115-5132
  • Cervical Cancer Screening JOURNAL OF THE NATIONAL COMPREHENSIVE CANCER NETWORK Partridge, E. E., Abu-Rustum, N. R., Campos, S. M., Fahey, P. J., Farmer, M., Garcia, R. L., Giuliano, A., Jones, H. W., Lele, S. M., Lieberman, R. W., Massad, S. L., Morgan, M. A., Reynolds, R. K., Rhodes, H. E., Singh, D. K., Smith-McCune, K., Teng, N., Trimble, C. L., Valea, F., Wilczynski, S. 2010; 8 (12): 1358-1386

    View details for Web of Science ID 000285132200006

    View details for PubMedID 21147902

  • Acoustic Analogy Formulations Accelerated by Fast Multipole Method for Two-Dimensional Aeroacoustic Problems AIAA JOURNAL Wolf, W. R., Lele, S. K. 2010; 48 (10): 2274-2285

    View details for DOI 10.2514/1.J050338

    View details for Web of Science ID 000282675700010

  • Large-Eddy Simulation of Jet Mixing in Supersonic Crossflows 19th AIAA Computational Fluid Dynamics Conference Kawai, S., Lele, S. K. AMER INST AERONAUT ASTRONAUT. 2010: 2063–83

    View details for DOI 10.2514/1.J050282

    View details for Web of Science ID 000281548100018

  • Investigation and modeling of bubble-bubble interaction effect in homogeneous bubbly flows PHYSICS OF FLUIDS Seo, J. H., Lele, S. K., Tryggvason, G. 2010; 22 (6)

    View details for DOI 10.1063/1.3432503

    View details for Web of Science ID 000280143100015

  • Large eddy simulation of free-stream turbulence effects on heat transfer to a high-pressure turbine cascade JOURNAL OF TURBULENCE Bhaskaran, R., Lele, S. K. 2010; 11 (6): 1-15
  • Assessment of localized artificial diffusivity scheme for large-eddy simulation of compressible turbulent flows JOURNAL OF COMPUTATIONAL PHYSICS Kawai, S., Shankar, S. K., Lele, S. K. 2010; 229 (5): 1739-1762
  • Assessment of high-resolution methods for numerical simulations of compressible turbulence with shock waves JOURNAL OF COMPUTATIONAL PHYSICS Johnsen, E., Larsson, J., Bhagatwala, A. V., Cabot, W. H., Moin, P., Olson, B. J., Rawat, P. S., Shankar, S. K., Sjoegreen, B., Yee, H. C., Zhong, X., Lele, S. K. 2010; 229 (4): 1213-1237
  • Compact adaptive-grid scheme for high numerical resolution simulations of isotachophoresis JOURNAL OF CHROMATOGRAPHY A Bercovici, M., Lele, S. K., Santiago, J. G. 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

  • Effect of transport modeling on hypersonic cooled wall boundary layer stability 7th IUTAM Symposium on Laminar-Turbulent Transition Franko, K., Lele, S. SPRINGER. 2010: 489–492
  • Large-eddy simulations of perfectly-expanded supersonic jets: quality assessment and validation Mendez, S., Shoeybi, M., Sharma, A., Ham, F., Lele, S., K., Moin, P. 2010
  • Large eddy simulation of an oblique shock impinging on a turbulent boundary layer Morgan, B., Kawai, S., Lele, S., K. 2010
  • Numerical simulation of multicomponent shock accelerated flows and mixing using localized artificial diffusivity method Shankar, S., Kawai, S., Lele, S., K. 2010
  • Far-field filtering and source-imaging for the study of jet noise Koenig, M., Cavalieri, A., Jordan, P., Papamoschou, D., Samimy, M., Lele, S. 2010
  • Fast acoustic scattering simulations with non-uniform potential flow effects Wolf, W., Lele, S., K. 2010
  • Effect of chemistry modeling on hypersonic boundary layer linear stability prediction Franko, K., Lele, S., K., MacCormack, R., W. 2010
  • Parameterization of subgrid plume dilution for use in large-scale atmospheric simulations ATMOSPHERIC CHEMISTRY AND PHYSICS Naiman, A. D., Lele, S. K., Wilkerson, J. T., Jacobson, M. Z. 2010; 10 (5): 2551-2560
  • Analysis of emission data from global commercial aviation: 2004 and 2006 ATMOSPHERIC CHEMISTRY AND PHYSICS Wilkerson, J. T., Jacobson, M. Z., Malwitz, A., Balasubramanian, S., Wayson, R., Fleming, G., Naiman, A. D., Lele, S. K. 2010; 10 (13): 6391-6408
  • UNSTRUCTURED LARGE EDDY SIMULATION TECHNOLOGY FOR PREDICTION AND CONTROL OF JET NOISE ASME Turbo Expo 2010 Khalighi, Y., Ham, F., Moin, P., Lele, S. K., Colonius, T., Schlinker, R. H., Reba, R. A., Simonich, J. AMER SOC MECHANICAL ENGINEERS. 2010: 57–70
  • Sources of high-speed jet noise: analysis of LES data and modeling IUTAM Symposium on Computational Aero-Acoustics for Aircraft Noise Prediction Lele, S. K., Mendez, S., Ryu, J., Nichols, J., Shoeybi, M., Moin, P. ELSEVIER SCIENCE BV. 2010: 84–93
  • Direct numerical simulation of canonical shock/turbulence interaction PHYSICS OF FLUIDS Larsson, J., Lele, S. K. 2009; 21 (12)

    View details for DOI 10.1063/1.3275856

    View details for Web of Science ID 000273216700027

  • The dynamics of nonlinear instability waves in laminar heated and unheated compressible mixing layers PHYSICS OF FLUIDS Cheung, L. C., Lele, S. K. 2009; 21 (9)

    View details for DOI 10.1063/1.3232329

    View details for Web of Science ID 000270378600033

  • A modified artificial viscosity approach for compressible turbulence simulations JOURNAL OF COMPUTATIONAL PHYSICS Bhagatwala, A., Lele, S. K. 2009; 228 (14): 4965-4969
  • On the growth and propagation of linear instability waves in compressible turbulent jets PHYSICS OF FLUIDS Ray, P. K., Cheung, L. C., Lele, S. K. 2009; 21 (5)

    View details for DOI 10.1063/1.3139302

    View details for Web of Science ID 000266500500029

  • Linear and nonlinear processes in two-dimensional mixing layer dynamics and sound radiation JOURNAL OF FLUID MECHANICS Cheung, L. C., Lele, S. K. 2009; 625: 321-351
  • Open source simulation tool for electrophoretic stacking, focusing, and separation JOURNAL OF CHROMATOGRAPHY A Bercovici, M., Lele, S. K., Santiago, J. G. 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

  • Numerical Experiments with Shock-Turbulence Interaction 3rd International Conference on Numerical Modeling of Space Plasma Flows Lele, S. K., Larsson, J., Bhagatwala, A., Moin, P. ASTRONOMICAL SOC PACIFIC. 2009: 31–41
  • LES of compressible turbulent flows: assessment of compact differencing with localized artificial diffusivity scheme Kawai, S., Shankar, S., K., Lele, S., K. 2009
  • Assessment of fast multipole method formulations for acoustic scattering Wolf, W., Lele, S., K. 2009
  • Noise predictions from cold high-speed turbulent jets using large-eddy simulation Ham, F., Sharma, A., Shoeybi, M., Lele, S., K., Moin, P., van der Weide, E. 2009
  • Fast field solutions in acoustic analogy formulations Wolf, W., Lele, S., K. 2009
  • Direct numerical simulations of canonical shock/turbulence interaction Larsson, J., Lele, S., K. 2009
  • A low-order contrail model to use with global-scale climate models Naiman, A., D., Lele, S., K., Wilkerson, J., T., Jacobson, M., Z. 2009
  • Numerical experiments with shock-turbulence interaction Lele, S., K., Larsson, J., Bhagatwala, A., Moin, P. edited by Pogorelov, Nikolai, V., Audit, E., Colella, P. 2009
  • Shock-turbulence Interaction: What we know and what we can learn from peta-scale Simulations Lele, S., K., Larsson, J. 2009
  • Large eddy simulation of free-stream turbulence effects on heat-transfer to a high pressure turbine cascade Bhaskaran, R., Lele, S., K. 2009
  • Shock-turbulence interaction: What we know and what we can learn from peta-scale simulations 5th Annual Conference of Scientific Discovery through Advanced Computing (SciDAC 2009) Lele, S. K., Larsson, J. IOP PUBLISHING LTD. 2009
  • Low-frequency sound sources in high-speed turbulent jets JOURNAL OF FLUID MECHANICS Bodony, D. J., Lele, S. K. 2008; 617: 231-253
  • Localized artificial diffusivity scheme for discontinuity capturing on curvilinear meshes JOURNAL OF COMPUTATIONAL PHYSICS Kawai, S., Lele, S. K. 2008; 227 (22): 9498-9526
  • Computational framework for coupling compressible and low Mach number codes AIAA JOURNAL Peet, Y. V., Lele, S. K. 2008; 46 (8): 1990-2001

    View details for DOI 10.2514/1.32884

    View details for Web of Science ID 000258281400010

  • Evolution of isolated turbulent trailing vortices PHYSICS OF FLUIDS Duraisamy, K., Lele, S. K. 2008; 20 (3)

    View details for DOI 10.1063/1.2840200

    View details for Web of Science ID 000254537600024

  • Current status of jet noise predictions using large-eddy simulation AIAA 44th Aerospace Sciences Meeting and Exhibit Bodony, D. J., Lele, S. K. AMER INST AERONAUT ASTRONAUT. 2008: 364–80

    View details for DOI 10.2514/1.24475

    View details for Web of Science ID 000252822800008

  • NEAR FIELD OF FILM COOLING JET ISSUED INTO A FLAT PLATE BOUNDARY LAYER: LES STUDY 53rd ASME Turbo Expo 2008 Peet, Y. V., Lele, S. K. AMER SOC MECHANICAL ENGINEERS. 2008: 409–418
  • Sound generation due to transient motion of a bluff body: direct computation and acoustic analogy predictions Sharma, A., Lele, S., K. 2008
  • Simulation strategies for shock-turbulence interaction Cook, A., W., Larsson, J., Cabot, W., H., Lele, S., K. 2008
  • Development of large eddy simulation for aero-thermal prediction in high-pressure turbine cascade Bhaskaran, R., Lele, S., K. 2008
  • Mechanisms of jet mixing in a supersonic crossflow: a study using large-eddy simulation Kawai, S., Lele, S., K. 2008
  • Fast multipole boundary element method for sound scattering from aerodynamic bodies Wolf, W., R., Lele, S., K. 2008
  • Investigation of the role of instability waves in jet noise radiation Ryu, J., Lele, S., K., Viswanathan, K. 2008
  • Toward petascale shock/turbulence computations 4th Annual Scientific Discovery Through Advanced Computing Conference (SciDAC 2008) Larsson, J., Johnsen, E., Lele, S. K., Moin, P. IOP PUBLISHING LTD. 2008
  • Stagnation-point flow under free-stream turbulence JOURNAL OF FLUID MECHANICS Xiong, Z., Lele, S. K. 2007; 590: 1-33
  • Sound generated by instability wave/shock-cell interaction in supersonic jets JOURNAL OF FLUID MECHANICS Ray, P. K., Lele, S. K. 2007; 587: 173-215
  • Interaction of vortex wakes and buoyant jets: A study of two-dimensional dynamics PHYSICS OF FLUIDS Shirgaonkar, A. A., Lele, S. K. 2007; 19 (8)

    View details for DOI 10.1063/1.2753515

    View details for Web of Science ID 000249156500044

  • An artificial nonlinear diffusivity method for supersonic reacting flows with shocks JOURNAL OF COMPUTATIONAL PHYSICS Fiorina, B., Lele, S. K. 2007; 222 (1): 246-264
  • Leading-edge effects in bypass transition JOURNAL OF FLUID MECHANICS Nagarajan, S., Lele, S. K., FERZIGER, J. H. 2007; 572: 471-504
  • Computational issues and algorithm assessment for shock/turbulence interaction problems 3rd Annual Scientific Discovery through Advanced Computing Conference (SciDAC 2007) Larsson, J., Cook, A., Lele, S. K., Moin, P., Cabot, B., Sjoegreen, B., Yee, H., Zhong, X. IOP PUBLISHING LTD. 2007
  • Computational issues and algorithm assessment for shock-turbulence interaction problems Larsson, J., Cook, A., Lele, S., K., Moin, P., Cabot, B., Sjogreen, B. 2007
  • Noise radiation predictions from jet instability waves using a hybrid nonlinear PSE-acoustic analogy Cheung, L., C., Bodony, D., J., Lele, S., K. 2007
  • Identification of instability waves in high speed turbulent jets Ryu, J., Lele, S., K., Viswanathan, K. 2007
  • Robustness of acoustic analogies for predicting mixing-layer noise AIAA JOURNAL Samanta, A., Freund, J. B., Wei, M., Lele, S. K. 2006; 44 (11): 2780-2786

    View details for DOI 10.2514/1.22186

    View details for Web of Science ID 000241851100041

  • Computational acoustics in spherical geometry: Steps toward validating helioseismology ASTROPHYSICAL JOURNAL Hanasoge, S. M., Larsen, R. M., Duvall, T. L., DeRosa, M. L., Hurlburt, N. E., Schou, J., Roth, M., Christensen-Dalsgaard, J., Lele, S. K. 2006; 648 (2): 1268-1275
  • On the extension of the Boussinesq approximation for inertia dominated flows PHYSICS OF FLUIDS Shirgaonkar, A. A., Lele, S. K. 2006; 18 (6)

    View details for DOI 10.1063/1.2206188

    View details for Web of Science ID 000238731500034

  • LARGE EDDY SIMULATION OF FILM COOLING FLOW ABOVE A FLAT PLATE FROM INCLINED CYLINDRICAL HOLES 2nd US-European Fluids Engineering Division Summer Meeting/14th International Conference on Nuclear Engineering Iourokina, I. V., Lele, S. K. AMER SOC MECHANICAL ENGINEERS. 2006: 817–825
  • Investigating broadband shock-associated noise of axisymmetric jets using large-eddy simulation Bodony, D., J., Ryu, J., Lele, S., K. 2006
  • Prediction of sound generated by a pitching airfoil: a comparison of RANS and LES Nagarajan, S., Hahn, S., Lele, S., K. 2006
  • On extension of the Boussinesq approximation for inertia dominated flows Phys. Fluids Shirgaonkar, A., Lele, S., K. 2006; 18: 066601, (12 pages)
  • Review of the current status of jet noise predictions using large-eddy simulation Bodony, D., J., Lele, S., K. 2006
  • Numerical investigations of a transverse jet in a supersonic crossflow using large-eddy simulation Fiorina, B., Lele, S., K. 2006
  • Large-eddy simulation of film-cooling flow above a flat plate from inclined cylindrical holes Iourokina, I., Lele, S., K. 2006
  • Far-field Jet Acoustics LES for Acoustics Bodony, D., J., Lele, S., K. edited by Wagner, C., Hutt, T., Sagaut, P. Cambridge University Press.. 2006: 1
  • Large-eddy simulation of film-cooling flows in a model turbine blade leading edge Iourokina, I., Lele, S., K. 2006
  • Large-eddy simulations of early stage contrails: effect of atmospheric properties Shirgaonkar, A., Lele, S., K. 2006
  • Sound generated by instability wave/shock-cell interaction in supersonic jets Ray, P., Lele, S., K. 2006
  • Computational prediction of flow-generated sound ANNUAL REVIEW OF FLUID MECHANICS Wang, M., Freund, J. B., Lele, S. K. 2006; 38: 483-512
  • On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets (vol 17, pg 085103, 2005) PHYSICS OF FLUIDS Bodony, D. J., Lele, S. K. 2005; 17 (11)

    View details for DOI 10.1063/1.2131828

    View details for Web of Science ID 000233603000044

  • Receptivity of the compressible mixing layer JOURNAL OF FLUID MECHANICS Barone, M. F., Lele, S. K. 2005; 540: 301-335
  • On using large-eddy simulation for the prediction of noise from cold and heated turbulent jets PHYSICS OF FLUIDS Bodony, D. J., Lele, S. K. 2005; 17 (8)

    View details for DOI 10.1063/1.2001689

    View details for Web of Science ID 000231392000028

  • New answers on the interaction between polymers and vortices in turbulent flows FLOW TURBULENCE AND COMBUSTION Dubief, Y., Terrapon, V. E., White, C. M., Shaqfeh, E. S., Moin, P., Lele, S. K. 2005; 74 (4): 311-329
  • Convective and absolute electrokinetic instability with conductivity gradients JOURNAL OF FLUID MECHANICS Chen, C. H., Lin, H., Lele, S. K., Santiago, J. G. 2005; 524: 263-303
  • Direct numerical simulation of polymer-induced drag reduction in turbulent boundary layer flow PHYSICS OF FLUIDS Dimitropoulos, C. D., Dubief, Y., Shaqfeh, E. S., Moin, P., Lele, S. K. 2005; 17 (1)

    View details for DOI 10.1063/1.1829751

    View details for Web of Science ID 000226358000005

  • Phased-array models of shock-cell noise sources Lele, S., K. 2005
  • Towards large-eddy simulation of film-cooling flows in a model turbine blade leading edge Iourokina, I., Lele, S., K. 2005
  • Sound generation by unsteady airfoil motions: a study using direct computation and acoustic analogy Nagarajan, S., Lele, S., K. 2005
  • Generation of low frequency sound in turbulent jets Bodony, D., J., Lele, S., K. 2005
  • Simulations of aircraft wake-exhaust mixing using LES: contrail formation in the near-field Shirgaonkar, A., Lele, S., K. 2005
  • Aeroacoustics of high-speed jets: a perspective from numerical simulations Lele, S., K. edited by Humphrey, J., Gatski, T. 2005
  • High-speed jet aeroacoustics: a perspective from numerical simulations Lele, S., K. edited by Humphrey, J., Gatski, T. 2005
  • Spatio-temporal multi-scale PSE for shear layer dynamics and acoustic radiation Cheung, L., C., Lele, S., K. 2005
  • Distortion of upstream disturbances in a Hiemenz boundary layer JOURNAL OF FLUID MECHANICS Xiong, Z. M., Lele, S. K. 2004; 519: 201-232
  • On the computation of space-time correlations by large-eddy simulation PHYSICS OF FLUIDS He, G. W., Wang, M., Lele, S. K. 2004; 16 (11): 3859-3867

    View details for DOI 10.1063/1.1779251

    View details for Web of Science ID 000224456800006

  • Simple method for generating inflow turbulence AIAA JOURNAL Xiong, Z., Nagarajan, S., Lele, S. K. 2004; 42 (10): 2164-2166
  • On the coherent drag-reducing and turbulence-enhancing behaviour of polymers in wall flows JOURNAL OF FLUID MECHANICS Dubief, Y., White, C. M., Terrapon, V. E., Shaqfeh, E. S., Moin, P., Lele, S. K. 2004; 514: 271-280
  • Computational aeroacoustics: progress on nonlinear problems of sound generation PROGRESS IN AEROSPACE SCIENCES Colonius, T., Lele, S. K. 2004; 40 (6): 345-416
  • Simulated polymer stretch in a turbulent flow using Brownian dynamics JOURNAL OF FLUID MECHANICS Terrapon, V. E., Dubief, Y., Moin, P., Shaqfeh, E. S., Lele, S. K. 2004; 504: 61-71
  • Jet noise prediction of cold and hot subsonic jets using large-eddy simulation Bodony, D., Lele, S., K. 2004
  • Acoustic radiation from subsonic and supersonic mixing layers with nonlinear PSE Cheung, Lawrence, C., Lele, S., K. 2004
  • Computational Aeroacoustics: a review of numerical approaches and progress in nonlinear problems of sound generation Progress in Aerospace Sciences Lele, S., K., Colonius, T. 2004; 6 (40): 345-416
  • On sound generated by instability wave-shock cell interaction in supersonic jets Ray, P., Cheung, Lawrence, C., Lele, S., K. 2004
  • Noise radiation from high-speed jets: Some insights from numerical simulations 5th International ERCOFTAC Workshop on Direct and Large-Eddy Simulation Lele, S. K. SPRINGER. 2004: 415–430
  • A robust high-order compact method for large eddy simulation JOURNAL OF COMPUTATIONAL PHYSICS Nagarajan, S., Lele, S. K., FERZIGER, J. H. 2003; 191 (2): 392-419
  • Shock leakage through an unsteady vortex-laden mixing layer: application to jet screech JOURNAL OF FLUID MECHANICS Suzuki, T., Lele, S. K. 2003; 490: 139-167
  • Direct numerical simulation of stagnation region flow and heat transfer with free-stream turbulence PHYSICS OF FLUIDS Bae, S. W., Lele, S. K., Sung, H. J. 2003; 15 (6): 1462-1484

    View details for DOI 10.1063/1.1565332

    View details for Web of Science ID 000182795300012

  • Green's functions for a source in a mixing layer: direct waves, refracted arrival waves and instability waves JOURNAL OF FLUID MECHANICS Suzuki, T., Lele, S. K. 2003; 477: 89-128
  • Green's functions for a source in a boundary layer: direct waves, channelled waves and diffracted waves JOURNAL OF FLUID MECHANICS Suzuki, T., Lele, S. K. 2003; 477: 129-173
  • Application of Adjoint Solutions to the Receptivity Problem in Compressible Mixing Layers Barone, M., F., Lele, S., K. 2003
  • Simulation and analogies of stagnation point heat transfer under free-stream turbulence Xiong, Z., Lele, S., K. 2003
  • The noise radiated by high-speed jets: some insights from numerical simulations Lele, S., K. 2003
  • Sound Generation Mechanism of Shock-Associated Noise Lui, C., Lele, S., K. 2003
  • A Statistical Subgrid Scale Noise Model: Formulation Bodony, D., Lele, S., K. 2003
  • A highly accurate technique for the treatment of flow equations at the polar axis in cylindrical coordinates using series expansions JOURNAL OF COMPUTATIONAL PHYSICS Constantinescu, G. S., Lele, S. K. 2002; 183 (1): 165-186
  • Refracted arrival waves in a zone of silence from a finite thickness mixing layer JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA Suzuki, T., Lele, S. K. 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 Barone, M., F., Lele, S., K. 2002
  • A numerical study of broad-band shock noise Lui, C., Lele, S., K. 2002
  • Numerical simulation of trailing edge receptivity Barone, M., F., Lele, S., K. 2002
  • Spatial scale decomposition of shear layer turbulence and the sound sources associated with the missing scales in a large-eddy simulation Bodony, D., J., Lele, S., K. 2002
  • A numerical investigation of broad-band shock noise Lui, C., Lele, S., K. 2002
  • Thermal perturbation of trailing vortices Euromech Colloquium 396 Orlandi, P., Carnevale, G. F., Lele, S. K., Shariff, K. GAUTHIER-VILLARS/EDITIONS ELSEVIER. 2001: 511–24
  • Vortex-wake pollution: A problem in fluid mechanics Symposium on Fluid Mechanics and the Environment held in Honor of Sidney Leibovich Lele, S. K. SPRINGER-VERLAG BERLIN. 2001: 163–181
  • Computational Aeroacoustics 2001 Yearbook of Science and Technology Lele, S., K. Mc Graw Hill. 2001: 107–111
  • Numerical study of leading edge heat transfer under free-stream turbulence Xiong, Z., Lele, S., K. 2001
  • Direct numerical simulation of spatially developing, compressible, turbulent mixing layers Lui, C., Lele, S., K. 2001
  • Computer Simulation and Prediction of Jet Noise High Speed Jet Flows Lele, S., K., Freund, J., B. edited by Raman, G., Mclaughlin, D., Morris, P. Taylor & Francis. 2001: 1
  • Computational Aeroacoustics for Jet Noise Physics Lele, S., K. 2001
  • Prediction of shock-cell structure using parabolized stability equations Choi, M., R., Lele, S., K. 2001
  • Computational Aeroacoustics 2001 Yearbook of Science and Technology Lele, S., K. 2001: 107-111
  • Large Eddy Simulation of a near sonic turbulent jet and its radiated noise Constantinescu, G., S., Lele, S., K. 2001
  • Shock leakage through an unsteady vortex-laden mixing layer: application to jet screech Suzuki, T., Lele, S., K. 2001
  • Computational Aeroacoustics for Jet Noise Physics Lele, S., K. edited by Lumley, J., L. 2001
  • Numerical simulation of a Mach 1.92 turbulent jet and its sound field AIAA/CEAS 4th Aeroacoustics Conference Freund, J. B., Lele, S. K., Moin, P. AMER INST AERONAUT ASTRONAUT. 2000: 2023–31
  • Compressibility effects in a turbulent annular mixing layer. Part 2. Mixing of a passive scalar JOURNAL OF FLUID MECHANICS Freund, J. B., Moin, P., Lele, S. K. 2000; 421: 269-292
  • Compressibility effects in a turbulent annular mixing layer. Part 1. Turbulence and growth rate JOURNAL OF FLUID MECHANICS Freund, J. B., Lele, S. K., Moin, P. 2000; 421: 229-267
  • Influence of inflow disturbances on stagnation-region heat transfer JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME Bae, S., Lele, S. K., Sung, H. J. 2000; 122 (2): 258-265
  • Computational Aeroacoustics: Recent Progress and Current Challenges Lele, S., K. 2000
  • Computational Aeroacoustics: Recent Progress and Current Challenges Lele, S., K. 2000
  • Direct numerical simulation of a low Reynolds number Mach 1.92 turbulent jet and its sound field AIAA Journal Freund, J., B., Lele, S., K., Moin, P. 2000; 38: 2023-2031
  • Green’s functions in a boundary layer: low and high frequency asymptotes Suzuki, T., Lele, S., K. 2000
  • Asymptotic growth of disturbances from spatially compact source in a skewed mixing layer PHYSICS OF FLUIDS Lu, G. Y., Lele, S. K. 1999; 11 (5): 1153-1160
  • Direct computation of the sound generated by vortex pairing in an axisymmetric jet JOURNAL OF FLUID MECHANICS Mitchell, B. E., Lele, S. K., Moin, P. 1999; 383: 113-142
  • Method for accelerating the destruction of aircraft wake vortices AIAA 36th Aerospace Sciences Meeting Rennich, S. C., Lele, S. K. AMER INST AERONAUT ASTRONAUT. 1999: 398–404
  • Receptivity to surface roughness near a swept leading edge JOURNAL OF FLUID MECHANICS Collis, S. S., Lele, S. K. 1999; 380: 141-168
  • Inviscid instability of compressible swirling mixing layers PHYSICS OF FLUIDS Lu, G. Y., Lele, S. K. 1999; 11 (2): 450-461
  • Direct numerical simulations of compressible turbulent flows: Fundamentals and applications 2nd ERCOFTAC Summer School on Turbulence and Transition Modelling Lele, S. K. SPRINGER. 1999: 421–488
  • Acoustic Scattering from a Mixing Layer: Role of Instability Waves Suzuki, T., Lele, S., K. 1999
  • A method for accelerating the destruction of aircraft-wake vortices Journal of Aircraft Rennich, S., C., Lele, S., K. 1999; 36: 398-404
  • Direct Numerical Simulation of Compressible Turbulent Flows: Fundamentals and Applications Turbulence and Combustion Modeling Lele, S., K. edited by Alfredsson, H., Johansson, A., Henningson, D. Kluwer Academic Publishing. 1999: 421–488
  • Large-Eddy Simulation of a Mach 0.9 Turbulent Jet Boersma, B., J., Lele, S., K. 1999
  • Numerical Simulation of Shock-Vortex Interaction in Supersonic Jet Screech Manning, T., Lele, S., K. 1998
  • Mechanism for Accelerating the Destruction of Aircraft Wake Vortices Rennich, S., C., Lele, S., K. 1998
  • Shock-vortex interactions in supersonic jet screech: an update Manning, T., A., Lele, S., K. 1998
  • Direct computation of Mach wave radiation in an axisymmetric supersonic jet AIAA JOURNAL Mitchell, B. E., Lele, S. K., Moin, P. 1997; 35 (10): 1574-1580
  • Numerical method for incompressible vortical flows with two unbounded directions JOURNAL OF COMPUTATIONAL PHYSICS Rennich, S. C., Lele, S. K. 1997; 137 (1): 101-129
  • Interaction of isotropic turbulence with shock waves: Effect of shock strength JOURNAL OF FLUID MECHANICS Lee, S. S., Lele, S. K., Moin, P. 1997; 340: 225-247
  • The influence of entropy fluctuations on the interaction of turbulence with a shock wave JOURNAL OF FLUID MECHANICS Mahesh, K., Lele, S. K., Moin, P. 1997; 334: 353-379
  • Sound generation in a mixing layer JOURNAL OF FLUID MECHANICS Colonius, T., Lele, S. K., Moin, P. 1997; 330: 375-409
  • Flows with density variations and compressibility: Similarities and differences IUTAM Symposium on Variable Density Low-Speed Turbulent Flows Lele, S. K. SPRINGER. 1997: 279–301
  • Computational Aeroacoustics: A Review invited lecture at the 35th Aerospace Sciences Meeting and Exhibit, AIAA Paper 97-0018 Lele, S., K. 1997
  • Direct Simulation of a Supersonic Round Turbulent Shear Layer Freund, J., B., Lele, S., K., Moin, P. 1997
  • Computational Aeroacoustics: A Review Lele, S., K. 1997
  • Computation of quadrupole noise using acoustic analogy AIAA JOURNAL Wang, M., Lele, S. K., Moin, P. 1996; 34 (11): 2247-2254
  • Sound radiation during local laminar breakdown in a low-Mach-number boundary layer JOURNAL OF FLUID MECHANICS Wang, M., Lele, S. K., Moin, P. 1996; 319: 197-218
  • Calculation of the radiated sound field using an open Kirchhoff surface AIAA JOURNAL Freund, J. B., Lele, S. K., Moini, P. 1996; 34 (5): 909-916
  • 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 Lele, S., K. 1996: 138-147
  • Sound Radiation During Local Laminar Breakdown in a Low Mach Number Boundary Layer Journal of Fluid Mechanics Wang, M., Lele, S., K., Moin, P. 1996; 319: 197-218
  • The Direct Computation of Mach Wave Radiation in an Axisymmetric Supersonic Jet Mitchell, B., E., Lele, S., K., Moin, P. 1996
  • Direct Numerical Simulation of the breakdown of Aircraft Wake Vortices Rennich, S., C., Lele, S., K. 1996
  • A Computational Approach to Swept Leading-Edge Receptivity Collis, S., S., Lele, S., K. 1996
  • Compressible and Hypersonic Flows Research Trends in Fluid Mechanics, Report by US National Committee for Theoretical and Applied Mechanics Lele, S., K. American Institute of Physics. 1996: 138–147
  • THE INTERACTION OF AN ISOTROPIC FIELD OF ACOUSTIC-WAVES WITH A SHOCK-WAVE JOURNAL OF FLUID MECHANICS Mahesh, K., Lee, S. S., Lele, S. K., Moin, P. 1995; 300: 383-407
  • DIRECT COMPUTATION OF THE SOUND FROM A COMPRESSIBLE CO-ROTATING VORTEX PAIR JOURNAL OF FLUID MECHANICS Mitchell, B. E., Lele, S. K., Moin, P. 1995; 285: 181-202
  • Direct Computation of the Sound Generated by Vortex Pairing in an Axisymmetric Jet Mitchell, B., E., Lele, S., K., Moin, P. 1995
  • The Sound Generated by a Two-Dimensional Shear Layer: A Comparison of Direct Computations and Acoustic Analogies Colonius, T., Lele, S., K., Moin, P. 1995
  • Calculation of the Radiated Sound Field Using an Open Kirchhoff Surface Freund, J., B., Lele, S., K., Moin, P. 1995
  • THE SCATTERING OF SOUND-WAVES BY A VORTEX - NUMERICAL SIMULATIONS AND ANALYTICAL SOLUTIONS JOURNAL OF FLUID MECHANICS Colonius, T., Lele, S. K., Moin, P. 1994; 260: 271-298
  • ON THE DENSITY RATIO EFFECT ON THE GROWTH-RATE OF A COMPRESSIBLE MIXING LAYER Symposium on Turbulence, in honor of the 60th Birthday of William Craig Reynolds Lu, G. Y., Lele, S. K. AMER INST PHYSICS. 1994: 1073–75
  • THE RESPONSE OF ANISOTROPIC TURBULENCE TO RAPID HOMOGENEOUS ONE-DIMENSIONAL COMPRESSION Symposium on Turbulence, in honor of the 60th Birthday of William Craig Reynolds Mahesh, K., Lele, S. K., Moin, P. AMER INST PHYSICS. 1994: 1052–62
  • COMPRESSIBILITY EFFECTS ON TURBULENCE ANNUAL REVIEW OF FLUID MECHANICS Lele, S. K. 1994; 26: 211-254
  • Interaction of Isotropic Turbulence With a Strong Shock Wave Lee, S., Lele, S., K., Moin, P. 1994
  • A Note on the Density Ratio Effect on the Growth Rate of a Compressible Mixing Layer The Physics of Fluids A Lu, G., Lele, S., K. 1994; 6: 1073-1075
  • Vortex Breakdown in Skewed Compressible Mixing Layers Lu, G., Lele, S., K. 1994
  • THE EVOLUTION OF A PLANE MIXING LAYER WITH SPANWISE NONUNIFORM FORCING PHYSICS OF FLUIDS Collis, S. S., Lele, S. K., Moser, R. D., Rogers, M. M. 1994; 6 (1): 381-396
  • BOUNDARY-CONDITIONS FOR DIRECT COMPUTATION OF AERODYNAMIC SOUND GENERATION AIAA JOURNAL Colonius, T., Lele, S. K., Moin, P. 1993; 31 (9): 1574-1582
  • DIRECT NUMERICAL-SIMULATION OF ISOTROPIC TURBULENCE INTERACTING WITH A WEAK SHOCK-WAVE JOURNAL OF FLUID MECHANICS Lee, S. S., Lele, S. K., Moin, P. 1993; 251: 533-562
  • VORTEX-INDUCED DISTURBANCE FIELD IN A COMPRESSIBLE SHEAR-LAYER PHYSICS OF FLUIDS A-FLUID DYNAMICS Papamoschou, D., Lele, S. K. 1993; 5 (6): 1412-1419
  • INVISCID INSTABILITY OF A SKEWED COMPRESSIBLE MIXING LAYER JOURNAL OF FLUID MECHANICS Lu, G. Y., Lele, S. K. 1993; 249: 441-463
  • Boundary Conditions for Direct Computation of Aerodynamic Sound Generation AIAA Journal Colonius, T., Lele, S., K., Moin, P. 1993; 31: 1574-1582
  • A Comparative Study of Turbulence Decay Using Navier-Stokes and a Discrete Particle Simulation Goswami, A., D., Baganoff, D., Lele, S., K., Feiereisen, W. 1993
  • Shock Turbulence Interaction in the Presence of Mean Shear: An Application of Rapid Distortion Theory Mahesh, K., Lele, S., K., Moin, P. 1993
  • Spatial Growth of Disturbances in a Skewed Compressible Mixing Layer Lu, G., Lele, S., K. 1993
  • Matching of Near/Far-field Equation Sets for Direct Computations of Aerodynamic Sound Freund, J., B., Lele, S., K., Moin, P. 1993
  • Direct Computation of the Sound Generated by a Two-Dimensional Shear Layer Colonius, T., Lele, S., K., Moin, P. 1993
  • SHOCK-JUMP RELATIONS IN A TURBULENT-FLOW PHYSICS OF FLUIDS A-FLUID DYNAMICS Lele, S. K. 1992; 4 (12): 2900-2905
  • COMPACT FINITE-DIFFERENCE SCHEMES WITH SPECTRAL-LIKE RESOLUTION JOURNAL OF COMPUTATIONAL PHYSICS Lele, S. K. 1992; 103 (1): 16-42
  • VORTICITY FORM OF TURBULENCE TRANSPORT-EQUATIONS PHYSICS OF FLUIDS A-FLUID DYNAMICS Lele, S. K. 1992; 4 (8): 1767-1772
  • BOUNDARY-CONDITIONS FOR DIRECT SIMULATIONS OF COMPRESSIBLE VISCOUS FLOWS JOURNAL OF COMPUTATIONAL PHYSICS Poinsot, T. J., Lele, S. K. 1992; 101 (1): 104-129
  • SIMULATION OF SPATIALLY EVOLVING TURBULENCE AND THE APPLICABILITY OF TAYLOR HYPOTHESIS IN COMPRESSIBLE FLOW PHYSICS OF FLUIDS A-FLUID DYNAMICS Lee, S., Lele, S. K., Moin, P. 1992; 4 (7): 1521-1530
  • Boundary Conditions for Direct Computations of Aerodynamic Sound Generation Colonius, T., Lele, S., K., Moin, P. 1992
  • Direct Computation of the Sound From a Compressible Co-rotating Vortex Pair Mitchell, B., E., Lele, S., K., Moin, P. 1992
  • THE FREE COMPRESSIBLE VISCOUS VORTEX JOURNAL OF FLUID MECHANICS Colonius, T., Lele, S. K., Moin, P. 1991; 230: 45-73
  • EDDY SHOCKLETS IN DECAYING COMPRESSIBLE TURBULENCE PHYSICS OF FLUIDS A-FLUID DYNAMICS Lee, S., Lele, S. K., Moin, P. 1991; 3 (4): 657-664
  • Motion of Particles With Inertia in a Compressible Free Shear Layer The Physics of Fluids A Samimy, M., Lele, S., K. 1991; 3: 1915-1923
  • Scattering of Sound Waves by a Compressible Vortex Colonius, T., Lele, S., K., Moin, P. 1991
  • Particle Laden Compressible Shear Layers Samimy, M., Lele, S., K. 1990
  • Nonlinear Dynamics in Langmuir Circulations and in Thermosolutal Convection Journal of Fluid Mechanics Leibovich, S., Lele, S., K., Moroz, I., M. 1989; 198: 471-511
  • Direct Numerical Simulation of Compressible Free Shear Flows Lele, S., K. 1989
  • A Consistency Condition for Reynolds Stress Closures Physics of Fluids Lele, S., K. 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 Leibovich, S., Lele, S., K. 1985; 150: 41-87
  • Direct Simulation of Shock-Turbulence Interaction Journal of Fluid Mechanics, 1993: corrigendum in Journal of Fluid Mechanics Lee, S., Lele, S., K., Moin, P. 1993, 1994; 251, 264: 373-374, 533-562
  • Evaluation of far-field sound using open surface corrections to Lighthill’s equation Cheung, L., C., Lele, S., K.
  • Parameterization of subgrid aircraft emission plumes for use in large-scale atmospheric simulations Atmos. Chem. Phys., also ATMOS. CHEM. PHYS. DISCUSS. Naiman, A., D., Lele, S., K., Wilkerson, J., T., Jacobson, M., Z. 2010, 2009; 10, 9: 2551-2560, 24755–24781
  • Direct Simulation of a Mach 1.92 Jet and its Sound Field Freund, J., B., Lele, S., K., Moin, P.
  • Direct Simulation and Analysis of Shock-turbulence Interaction Lee, S., Lele, S., K., Moin, P.