Particle rebound/deposition modelling in engine hot sections

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2022-80013
AuthorSearch for: 1ORCID identifier: https://orcid.org/0009-0008-0777-7919; Search for: ; Search for: 1ORCID identifier: https://orcid.org/0000-0002-2122-3882; Search for: 1
Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
ConferenceASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition, June 13-17, 2022, Rotterdam, Netherlands
Physical description14 p.
Subjectenvironmental particle; sand; rebound; deposition; gas turbine; hot-sections
Abstract
Publication date
PublisherAmerican Society of Mechanical Engineers
In
LanguageEnglish
Peer reviewedYes
IdentifierGT2022-80013, V10BT31A005
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Record identifier62333262-bf37-4225-84b3-739875c2eb79
Record created2024-11-13
Record modified2024-11-13
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