Aeroelastic assessment of a highly loaded high pressure compressor exposed to pressure gain combustion disturbances
A numerical aeroelastic assessment of a highly loaded high pressure compressor exposed to flow disturbances is presented in this paper. The disturbances originate from novel, inherently unsteady, pressure gain combustion processes, such as pulse detonation, shockless explosion, wave rotor or piston...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Global Power and Propulsion Society
2018-10-01
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| Series: | Journal of the Global Power and Propulsion Society |
| Subjects: | |
| Online Access: | https://www.gppsjournal.org/journals/journal-of-the-global-power-and-propulsion-society/aeroelastic-assessment-of-a-highly-loaded-high-pressure-compressor-exposed-to-pressure-gain-combustion-disturbances/ |