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Iterative Inverse Design Method with AUSM+-Up Scheme Implemented on Unstructured Grids
An iterative inverse design method is developed for obtaining the blade geometry that corresponds to the required pressure distribution. AUSM(+)-up scheme is used for flux computation and implemented on finite volume unstructured grid. The blade geometry is modified after certain iterations, and the...
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Published in: | Journal of propulsion and power 2012-01, Vol.28 (1), p.16-26 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | An iterative inverse design method is developed for obtaining the blade geometry that corresponds to the required pressure distribution. AUSM(+)-up scheme is used for flux computation and implemented on finite volume unstructured grid. The blade geometry is modified after certain iterations, and the spring analogy is used for mesh deformation after each modification. The robustness of the method is determined by verifying that the final blade geometry is independent of the initial choice of the blade profile. Results for a compressor cascade are presented in this paper. |
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ISSN: | 0748-4658 1533-3876 |
DOI: | 10.2514/1.B34216 |