Balancing configuration and refinement in the design of two-spool multistage compression systems
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
1528-8900
Volume Title
137
Publisher
ASME International
Publisher DOI
Sponsorship
The authors thank Rolls‐Royce plc for their support.