AbstractThis 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.
Preliminary study to raise axial flow compressors up to the context-awareness standards
Aerospace Science and Technology ; 12 , 7 ; 515-523
2007-12-21
9 pages
Article (Journal)
Electronic Resource
English
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|Reverse flow in multistage axial compressors
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|Aerodynamic design and axial flow compressors
SLUB | 1965
|Reverse flow in multistage axial compressors
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|