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A robust design optimization of a mixed-flow compressor impeller
Date
2009-06-08
Author
Çevik, Mert
Uzol, Oğuz
Yavrucuk, İlkay
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This paper presents the results of a design and optimization study for the impeller of a small mixed-flow compressor. The objective of the optimization is to obtain an impeller geometry that could minimize a cost function based on the specific thrust and the thrust specific fuel consumption (TSFC) of a small jet engine. The design methodology is based on generating a configurational database for various compressor geometries using ID design codes and a commercial turbomachinery design/analysis software, application of Design of Experiments to properly sample the design space, representing the cost function variations within the design space through a neural-network and then finding the optimum configuration that minimizes the cost function. A sample design optimization study showed that the designed compressor as well as the engine that it's designed for have improved performance characteristics when compared to a typical small turbojet engine and its small radial compressor.
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https://hdl.handle.net/11511/82170
http://apps.webofknowledge.com/full_record.do?product=WOS&search_mode=GeneralSearch&qid=9&SID=F6Kz86idFC1LYa3L9Ej&page=1&doc=4
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Department of Aerospace Engineering, Conference / Seminar
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M. Çevik, O. Uzol, and İ. Yavrucuk, “A robust design optimization of a mixed-flow compressor impeller,” 2009, p. 699, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/82170.
