Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718720 | Aerospace Science and Technology | 2008 | 9 Pages |
Abstract
This paper explains summary of a method to introduce context-awareness into gas turbine engines, which urges making essential changes in power transmission and compression process. Applying these changes on axial flow compressors enhances individual and free access to each component, and then conventional methods to design and model their characteristic map should be adapted aptly. Accordingly, suitable methodology is introduced, and based on that, an alternative to HPC of GE90-94B turbofan engine is designed and modeled by computer in average-fidelity level.
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