On the acoustic response of a generic gas turbine fuel injector passage
A current trend in the design of modern aero engines is the transition towards leaner combustion as a solution to satisfy increasingly stringent emission regulations. Lean combustion systems are often more susceptible to thermoacoustic instability and the fuel injector can play a critical role. This...
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| Main Authors: | , , |
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| Format: | Default Article |
| Published: |
2019
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/36727 |
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