Gas turbine combustor modelling

Par Conseil national de recherches du Canada

Auteur	Rechercher : Jiang, Lei-Yong¹Identifiant ORCID : https://orcid.org/0009-0008-0777-7919
Affiliation	Conseil national de recherches du Canada. Aérospatiale
Format	Texte, Livre
ISBN	978-6138930730 6138930738
Description physique	120 p.
Résumé	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.
Date de publication	2020-07-13
Maison d’édition	Scholar's Press
Langue	anglais
Publications évaluées par des pairs	Oui
Exporter la notice	Exporter en format RIS
Signaler une correction	Signaler une correction (s'ouvre dans un nouvel onglet)
Identificateur de l’enregistrement	ef01788d-d1d4-49ce-b309-f9a96464cf03
Enregistrement créé	2024-11-28
Enregistrement modifié	2024-11-28

Date de modification :: 2025-05-09