Sanjiva Lele
 Professor
                            Aeronautics and Astronautics                                                        
Stanford University
                                                        United States of America
                        
Biography
Sanjiva Lele is working as Professor, Aeronautics and Astronautics and Mechanical Engineering Stanford University. Member of Bio-X. Received 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), Stanford Asian American Faculty Award, Stanford Asian American Faculty (2004).
Research Interest
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
Publications
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AL Bernardini M, Pirozzoli S, Orlandi P, Lele SK (2014) Parameterization of Boundary-Layer Transition Induced by Isolated Roughness Elements. AIAA JOURN 52: 2261-2269
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Ryu J, Lele SK, Viswanathan K (2014) Study of supertonic wave components in high-speed turbulent jets using an LES database JOURNAL OF SOUND AND VIBRATION 333: 6900-6923
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Ryu J, Lele SK (2015) Instability waves in high-speed jets: near-and far-field DNS/LES data analysis. INTERNATIONAL JOURNAL OF AEROACOUSTICS 14: 643-673.