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Gas turbine combustor modelling

From National Research Council Canada

AuthorSearch for: 1ORCID identifier: https://orcid.org/0009-0008-0777-7919
Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Book
ISBN978-6138930730
6138930738
Physical description120 p.
Abstract
The combustor is one of the four major engine components and is directly associated with engine performance such as the efficiency, emissions, safety, and economy. To simulate combustion systems properly, advanced knowledge or expertise in combustion theory and modeling is required. Simply running “off-the-shelf” software without a deep understanding of numerical methods and physical models can be dangerous. Considering the many-faceted criteria and enormous risks related to the design of combustion systems, this requirement is imperative. This book is based on the author’s work on the gas turbine combustor modeling over more than a decade. The contents should serve as good references for engineers and researchers in the development and maintenance of gas turbine engines, and useful learning materials to students who wish to work in this field. Most of the contents are also suitable to engineers and researchers working with other types of combustion systems.
Publication date
PublisherScholar's Press
LanguageEnglish
Peer reviewedYes
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Record identifieref01788d-d1d4-49ce-b309-f9a96464cf03
Record created2024-11-28
Record modified2024-11-28
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