TY - GEN
T1 - The Pele Simulation Suite for Reacting Flows at Exascale
AU - Henry de Frahan, Marc T.
AU - Esclapez, Lucas
AU - Rood, Jon
AU - Wimer, Nicholas T.
AU - Mullowney, Paul
AU - Perry, Bruce A.
AU - Owen, Landon
AU - Sitaraman, Hariswaran
AU - Yellapantula, Shashank
AU - Hassanaly, Malik
AU - Rahimi, Mohammad J.
AU - Martin, Michael J.
AU - Doronina, Olga A.
AU - Sreejith, N. A.
AU - Rieth, Martin
AU - Ge, Wenjun
AU - Sankaran, Ramanan
AU - Almgren, Ann S.
AU - Zhang, Weiqun
AU - Bell, John B.
AU - Grout, Ray
AU - Day, Marc S.
AU - Chen, Jacqueline H.
N1 - Publisher Copyright:
Copyright © 2024 "MMJBODF GPS 4VTUBJOBCMF &OFSHZ -$
PY - 2024
Y1 - 2024
N2 - In this work, we present the Pele suite of software tools for compressible and incompressible reacting flows. The Pele suite leverages several different libraries, notably AMReX and SUNDIALS, to achieve performance portability on heterogeneous computing architectures across the supercomputing landscape. The Pele suite is comprised of PeleC, a compressible reacting flow block-structured adaptive mesh refinement solver, PeleLMeX, a low-Mach number reacting flow block-structured adaptive mesh refinement solver, PelePhysics, a library for transport, thermodynamics, finite rate chemistry, soot, spray and radiation physics. The objective of this paper is (i) to present the code development efforts necessary to achieve highly effective and scalable applications for exascale machines and (ii) to detail the performance results of the Combustion-Pele project applications on Oak Ridge National Laboratory’s Frontier. We show good weak and strong scaling results for both PeleC and PeleLMeX up to more than 50 billion cells on more than 4096 Frontier graphics processing unit nodes. We also present a capability demonstration simulation of a dual-fuel pulse compression ignition engine (six adaptive mesh refinement levels, and 60 billion cells or 2.1 trillion degrees of freedom) on Frontier, to date one of the largest simulations performed on the first exascale-class supercomputer.
AB - In this work, we present the Pele suite of software tools for compressible and incompressible reacting flows. The Pele suite leverages several different libraries, notably AMReX and SUNDIALS, to achieve performance portability on heterogeneous computing architectures across the supercomputing landscape. The Pele suite is comprised of PeleC, a compressible reacting flow block-structured adaptive mesh refinement solver, PeleLMeX, a low-Mach number reacting flow block-structured adaptive mesh refinement solver, PelePhysics, a library for transport, thermodynamics, finite rate chemistry, soot, spray and radiation physics. The objective of this paper is (i) to present the code development efforts necessary to achieve highly effective and scalable applications for exascale machines and (ii) to detail the performance results of the Combustion-Pele project applications on Oak Ridge National Laboratory’s Frontier. We show good weak and strong scaling results for both PeleC and PeleLMeX up to more than 50 billion cells on more than 4096 Frontier graphics processing unit nodes. We also present a capability demonstration simulation of a dual-fuel pulse compression ignition engine (six adaptive mesh refinement levels, and 60 billion cells or 2.1 trillion degrees of freedom) on Frontier, to date one of the largest simulations performed on the first exascale-class supercomputer.
UR - http://www.scopus.com/inward/record.url?scp=85193569973&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85193569973
T3 - 2024 SIAM Conference on Parallel Processing for Scientific Computing, PP 2024
SP - 13
EP - 25
BT - 2024 SIAM Conference on Parallel Processing for Scientific Computing, PP 2024
A2 - Bader, Michael
A2 - Dubey, Anshu
A2 - Lusch, Bethany
PB - Society for Industrial and Applied Mathematics Publications
T2 - 22nd SIAM Conference on Parallel Processing for Scientific Computing, PP 2024
Y2 - 5 March 2024 through 8 March 2024
ER -