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Balancing configuration and refinement in the design of two-spool multistage compression systems


Type

Article

Change log

Authors

Jarrett, JP 
Ghisu, T 

Abstract

jats:pWith limited resources, time spent refining a design is time not spent in selecting its optimal configuration. A multi-fidelity optimization scheme is applied to the configuration and refinement of a generic core engine compression system. The best designs result from expending between half and three quarters of the total design effort on configuration selection. The performance of the refinement phase is a weak function of the preceding configuration phase when the latter is well into diminishing returns. By exploiting this behavior, the time taken to obtain equally good designs with the same analysis tools and computational resource may be halved.</jats:p>

Description

Keywords

4012 Fluid Mechanics and Thermal Engineering, 40 Engineering, 4001 Aerospace Engineering

Journal Title

Journal of Turbomachinery

Conference Name

Journal ISSN

0889-504X
1528-8900

Volume Title

137

Publisher

ASME International
Sponsorship
The authors thank Rolls‐Royce plc for their support.