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NASA NTRS · 19940023678

High-performance parallel analysis of coupled problems for aircraft propulsion

Abstract

Applications are described of high-performance parallel, computation for the analysis of complete jet engines, considering its multi-discipline coupled problem. The coupled problem involves interaction of structures with gas dynamics, heat conduction and heat transfer in aircraft engines. The methodology issues addressed include: consistent discrete formulation of coupled problems with emphasis on coupling phenomena; effect of partitioning strategies, augmentation and temporal solution procedures; sensitivity of response to problem parameters; and methods for interfacing multiscale discretizations in different single fields. The computer implementation issues addressed include: parallel treatment of coupled systems; domain decomposition and mesh partitioning strategies; data representation in object-oriented form and mapping to hardware driven representation, and tradeoff studies between partitioning schemes and fully coupled treatment.

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BibTeXRIS

Felippa, C. A., Farhat, C., Lanteri, S., Gumaste, U., Ronaghi, M.. 1994-03-01. High-performance parallel analysis of coupled problems for aircraft propulsion. https://ntrs.nasa.gov/citations/19940023678

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