Follow
Saurabh S. Sawant
Title
Cited by
Cited by
Year
Ablative thermal protection systems: Pyrolysis modeling by scale-bridging molecular dynamics
A Harpale, S Sawant, R Kumar, D Levin, HB Chew
Carbon 130, 315-324, 2018
532018
Application of adaptively refined unstructured grids in DSMC to shock wave simulations
SS Sawant, O Tumuklu, R Jambunathan, DA Levin
Computers & Fluids 170, 197-212, 2018
232018
Linear stability analysis of hypersonic boundary layers computed by a kinetic approach: A semi-infinite flat plate at 4.5≤ M∞≤ 9
A Klothakis, H Quintanilha Jr, SS Sawant, E Protopapadakis, V Theofilis, ...
Theoretical and Computational Fluid Dynamics 36 (1), 117-139, 2022
192022
On the synchronisation of three-dimensional shock layer and laminar separation bubble instabilities in hypersonic flow over a double wedge
SS Sawant, V Theofilis, DA Levin
Journal of Fluid Mechanics 941, A7, 2022
182022
Multi-scale thermal response modeling of an AVCOAT-like thermal protection material
SS Sawant, P Rao, A Harpale, HB Chew, DA Levin
International Journal of Heat and Mass Transfer 133, 1176-1195, 2019
162019
Study of particle lifting mechanisms in an electrostatic discharge plasma
AV Marayikkottu, SS Sawant, DA Levin, C Huang, M Schoenitz, ...
International Journal of Multiphase Flow 137, 103564, 2021
102021
Linear instability of shock-dominated laminar hypersonic separated flows
SS Sawant, O Tumuklu, V Theofilis, DA Levin
IUTAM Laminar-Turbulent Transition: 9th IUTAM Symposium, London, UK …, 2022
92022
A kinetic approach to studying low-frequency molecular fluctuations in a one-dimensional shock
SS Sawant, DA Levin, V Theofilis
Physics of Fluids 33 (10), 2021
82021
Slip effects on the stability of supersonic laminar flat plate boundary layer
A Klothakis, SS Sawant, H Quintanilha, V Theofilis, DA Levin
AIAA Scitech 2021 Forum, 1659, 2021
82021
High fidelity and multi-scale thermal response modeling of an Avcoat-like TPS
SS Sawant, A Harpale, R Jambunathan, H Beng Chew, DA Levin
55th AIAA Aerospace Sciences Meeting, 0438, 2017
72017
Analytical prediction of low-frequency fluctuations inside a one-dimensional shock
SS Sawant, DA Levin, V Theofilis
Theoretical and Computational Fluid Dynamics, 1-16, 2021
52021
Micro-scale thermal response modeling of Avcoat-like TPS
SS Sawant, P Rao, A Harpale, HB Chew, DA Levin
2018 AIAA Aerospace Sciences Meeting, 0495, 2018
52018
Study of shock-shock interactions using an unstructured amr octree dsmc code
SS Sawant, R Jambunathan, O Tumuklu, B Korkut, DA Levin
54th AIAA Aerospace Sciences Meeting, 0501, 2016
42016
Study of inert simulated particle transportation in a moving shock/pressure wave generated by electrostatic discharges
A Marayikkottu Vijayan, SS Sawant, P Rao, DA Levin
AIAA Scitech 2019 Forum, 0631, 2019
32019
Development of an amr octree dsmc approach for shock dominated flows
SS Sawant, B Korkut, O Tumuklu, DA Levin
53rd AIAA Aerospace Sciences Meeting, 0070, 2015
32015
Characterization of transmission lines in microelectronic circuits using the artemis solver
SS Sawant, Z Yao, R Jambunathan, A Nonaka
IEEE Journal on Multiscale and Multiphysics Computational Techniques 8, 31-39, 2022
22022
Comparison of numerical simulations of inert particle transport in an electrostatic discharge with experimental results
A Marayikkottu Vijayan, SS Sawant, DA Levin, C Huang, M Schoenitz, ...
AIAA Scitech 2020 Forum, 1798, 2020
22020
The development of kinetic models and simulation methods to study molecular fluctuations, modal response, and shock-laminar separation bubble instabilities
SS Sawant
University of Illinois at Urbana-Champaign, 2022
12022
The effect of an isolated cylindrical roughness element on a semi-infinite flat plate in rarefied Mach 6 flow is studied using Direct Simulation Monte Carlo methods
A Klothakis, K Dylewicz, V Theofilis, SS Sawant, DA Levin
AIAA AVIATION 2022 Forum, 4029, 2022
12022
On the effect of velocity slip and temperature jump on flat plate boundary layer stability at Mach 4.5
A Klothakis, H Quintanilha Jr, SS Sawant, E Protopapadakis, V Theofilis, ...
APS Division of Fluid Dynamics Meeting Abstracts, H05. 003, 2020
12020
The system can't perform the operation now. Try again later.
Articles 1–20