Influence of inlet swirl on pattern factor and pressure loss in an aero engine combustor
Author:
Affiliation:
1. Department of Mechanical Engineering, Indian Institute of Technology, Chennai, India
2. Aero Engine Research and Design Center, Hindustan Aeronautics Ltd., Bengaluru, India
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/09544062211027209
Reference15 articles.
1. Gas Turbine Combustion
2. Numerical study of effect of compressor swirling flow on combustor design in a MTE
3. Investigations of Combustor Inlet Swirl on the Liner Wall Temperature in an Aero Engine Combustor
4. Effects of Combustion Chamber Geometry Deviations Upon Exit Temperature Profiles for Populations With Varied Service Limitations
5. An investigation of air-swirl design criteria for gas turbine combustors through a multi-objective CFD optimization
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