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Optimization of Compressor Vane and Bleed Settings

Joseph E. Garberoglio

出版	Aero Propulsion Laboratory, Wright Aeronautical Laboratories, Air Force Systems Command, 1981
URL	http://books.google.com.hk/books?id=V2UMdMmpKiAC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

This report evaluates optimization methods for their effectiveness in relating multistage axial compressor test data to the decision to vary a selected vane or bleed to reach a predetermined performance goal. Compressor simulations were used in a comparative evaluation and each method was judged on the basis of the number of tests required to achieve an optimum performance goal. The influence of measurement errors and finite vane travel were also prime considerations. Based on this evaluation, the COPES/CONMIN approximate optimization technique was chosen most suitable. (Author).