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UID:221@cds.iisc.ac.in
DTSTART;TZID=Asia/Kolkata:20260821T140000
DTEND;TZID=Asia/Kolkata:20260821T150000
DTSTAMP:20260814T134013Z
URL:https://cds.iisc.ac.in/events/m-tech-research-thesis-defense-cds-async
 hronous-computing-and-low-precision-approaches-towards-accelerating-flow-s
 imulations/
SUMMARY:M.Tech Research Thesis Defense: CDS: "Asynchronous computing and lo
 w-precision approaches towards accelerating flow simulations"
DESCRIPTION:DEPARTMENT OF COMPUTATIONAL AND DATA SCIENCES\nM.Tech Research 
 Thesis Defense\n\n\n\nSpeaker : Mr. Aswin Kumar A\nS.R. Number : 06-18-01-
 10-22-24-1-24417\nTitle : "Asynchronous computing and low-precision approa
 ches towards accelerating flow simulations."\nThesis examiner : Prof. Ratn
 esh K. Shukla\, Mechanical Engineering\, IISc\nResearch Supervisor: Dr. Ko
 nduri Aditya\nDate &amp\; Time : August 21\, 2026\, 02:00 PM\nVenue : # 10
 2 CDS Seminar Hall\n\n\n\nABSTRACT\n\nThe increasing computational cost of
  high-fidelity flow simulations at extreme scales has made communication o
 verheads arising from data movement and synchronization a major bottleneck
  in modern high-performance computing. At the same time\, emerging GPU- an
 d TPU-based architectures provide significantly higher throughput for low-
 precision arithmetic compared to traditional double-precision computations
 . This thesis investigates asynchronous computing approaches and low-preci
 sion numerical frameworks towards accelerating compressible and reacting f
 low simulations on future exascale supercomputers.\n\nThe primary focus of
  this work is the development and evaluation of asynchronous numerical met
 hods that relax communication and synchronization at a mathematical level 
 while preserving the high-order accuracy of the underlying numerical schem
 es. Previously developed asynchrony-tolerant (AT) schemes are incorporated
  into the high-order compressible flow solver COMP-SQUARE in a multi-block
  framework for practically relevant flow problems in complex geometries. T
 wo asynchronous algorithms are considered: one that avoids communication o
 ver a few predetermined time steps\, and another that initiates communicat
 ion without enforcing synchronization. The numerical efficacy and scalabil
 ity of these asynchronous algorithms are demonstrated for several benchmar
 k problems\, including isentropic advection of a vortex\, the Taylor-Green
  vortex\, and the highly sensitive case of transitional flow over a NACA00
 12 airfoil. Scaling experiments performed on up to 18\,432 cores demonstra
 te speed-ups of up to four times with respect to the baseline synchronous 
 solver while maintaining solution accuracy. These results demonstrate the 
 applicability of AT schemes to established CFD solvers for improving scala
 bility at extreme scales.\n\nThis work further extends the asynchronous co
 mputing framework to discontinuous Galerkin (DG) methods for compressible 
 reacting flows. Although DG methods are attractive for their high arithmet
 ic intensity and their ability to accurately handle discontinuities such a
 s shocks and detonations\, their scalability is also limited by communicat
 ion bottlenecks arising from synchronization between processing elements (
 PEs). An asynchronous discontinuous Galerkin (ADG) method is developed for
  chemically reacting flows with detailed chemistry\, and new asynchrony-to
 lerant weighted essentially non-oscillatory (AT-WENO) limiters are propose
 d to accurately capture discontinuities in the presence of communication d
 elays near PE boundaries. The numerical properties of the ADG framework ar
 e evaluated for spontaneous ignition\, premixed flame propagation\, and de
 tonation-wave propagation on a one-dimensional domain. The asynchronous so
 lver accurately captures ignition fronts and discontinuities while incurri
 ng negligible numerical errors at PE boundaries. Preliminary scaling studi
 es further demonstrate the potential of the ADG method as a basis for high
 ly scalable DG-based solvers for massively parallel combustion simulations
 .\n\nIn addition to asynchronous algorithms\, this thesis also explores lo
 w-precision approaches for reacting-flow simulations motivated by the hard
 ware characteristics of modern accelerators. A low-precision framework is 
 investigated in which the chemical kinetics evaluations are performed in h
 alf precision (FP16)\, while the nonlinear temperature solve is performed 
 in higher precision. The framework is assessed using lean hydrogen-air aut
 oignition with detailed chemical kinetics. Predictions of ignition delay a
 nd the evolution of temperature\, heat-release rate\, and species mass fra
 ctions show excellent agreement with FP64 reference solutions over a range
  of conditions. These preliminary findings demonstrate the feasibility of 
 low-precision approaches for reacting-flow solvers while also identifying 
 important considerations regarding robustness and generalizability.\n\nOve
 rall\, this thesis demonstrates that asynchronous computing methodologies 
 and low-precision numerical approaches provide promising and complementary
  pathways towards improving the scalability and computational efficiency o
 f next-generation flow solvers for exascale scientific computing.\n\n\n\nA
 LL ARE WELCOME
CATEGORIES:Events,Thesis Defense
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