Design optimization of a mixed-flow compressor impeller for a small turbojet engine

Date

2011-01-01

Author

Cevik, Mert
Uzol, Oğuz

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Purpose - This paper aims to present the results of a design 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 of a small turbojet engine.

Subject Keywords

Jet engines, Optimum design, Compressors

URI

https://hdl.handle.net/11511/40368

Journal

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY

DOI

https://doi.org/10.1108/00022661111131212

Collections

Department of Aerospace Engineering, Article

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Citation Formats

M. Cevik and O. Uzol, “Design optimization of a mixed-flow compressor impeller for a small turbojet engine,” AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, pp. 127–137, 2011, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/40368.