A dual-mesh approach to enhance accuracy of the boundary conditions for unstructured grid modeling of turbomachinery flows

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2010-23390
AuthorSearch for: 1; Search for: 1ORCID identifier: https://orcid.org/0009-0008-0777-7919
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceASME Turbo Expo 2010: Power for Land, Sea, and Air, June 14-18, 2010, Glasgow, Scotland, United Kingdom
Subjectboundary-value problems; flow (dynamics); modeling; turbomachinery; inflow; outflow; computational fluid dynamics; algorithms; compressors; engineering systems and industry applications; turbines
Abstract
Publication date
PublisherAmerican Society of Mechanical Engineers
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LanguageEnglish
Peer reviewedYes
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