Flame initiation and development at sub-atmospheric conditions in aeronautical gas turbine combustors [Redacted version]

The introduction of sustainable aviation fuels and the imposed requirements to reduce NOx pro duction can impair the in-flight relight performance of a gas turbine combustor. The design of a combustor to meet ignition demands relies on the experience made with similar geometries due to the lack of e...

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Bibliographic Details
Main Author: Dimitri Franz
Format: Default Thesis
Published: 2023
Subjects:
Aerospace engineering not elsewhere classified
Automotive engineering not elsewhere classified
Relight
Ignition
Sub-atmospheric
RQL
Combustor
Gas turbine
Reduced-order model
Cantera
Online Access:https://dx.doi.org/10.26174/thesis.lboro.24474979.v1
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