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Section 17
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Interactive computing methods for aeroelastic analysis of turbomachinery
Article first published online: 22 DEC 2004
DOI: 10.1002/pamm.200410261
Copyright © 2004 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim
1617-7061/asset/cover.gif?v=1&s=79b6ccfe3470758033c99b476335ce58b5a38819 "PAMM")
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How to Cite
Dumitrache, A. (2004), Interactive computing methods for aeroelastic analysis of turbomachinery. Proc. Appl. Math. Mech., 4: 560–561. doi: 10.1002/pamm.200410261
Publication History
- Issue published online: 22 DEC 2004
- Article first published online: 22 DEC 2004
References
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- [2], Deforming grid variational principle for unsteady small disturbances flows in cascades, AIAA Journal 31, 891–900 (1993).
- [3], New quasi-simultaneous method to calculate interacting boundary layers, AIAA Journal 19, 79–85 (1981).