Parallelization of a three-dimensional flow solver for Euler rotorcraft aerodynamics predictions

DOI10.2514/3.13391zbMath0911.76050OpenAlexW2154035932MaRDI QIDQ3839620

Anastasios S. Lyrintzis, Roger C. Strawn, Andrew M. Wissink

Publication date: 16 May 1999

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/45289c8a282758d0e6647e64e49716660c20ee38

zbMATH Keywords

message passingdomain decomposition techniqueThinking Machines CM-5distributed-memory parallel architectureshelicopter rotor in forward flightIBMS SP2lower-upper symmetric Gauss-Seidel algorithmtransonic unsteady roter Navier-Stokes solver

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) General theory of rotating fluids (76U05) Parallel numerical computation (65Y05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10)

Related Items (6)

Acceleration on stretched meshes with line-implicit LU-SGS in parallel implementation ⋮ Parallel versions of implicit LU-SGS method ⋮ Flowmodellium software package for calculating high-speed flows of compressible fluid ⋮ Acceleration of the data-parallel lower-upper relaxation time-integration method on GPU for an unstructured CFD solver ⋮ A multithreaded OpenMP implementation of the LU-SGS method using the multilevel decomposition of the unstructured computational mesh ⋮ Short Communication: A Parallel Newton–Krylov Method for Navier–Stokes Rotorcraft Codes

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