Summary
A model reduction test case is presented, which considers flow through an actively controlled supersonic diffuser. The problem setup and computational fluid dynamic (CFD) model are described. Sample model reduction results for two transfer functions of interest are then presented.
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References
G. Lassaux. High-Fidelity Reduced-Order Aerodynamic Models: Application to Active Control of Engine Inlets. Master's thesis, Dept. of Aeronautics and Astronautics, MIT, June 2002.
G. Lassaux and K Willcox. Model reduction for active control design using multiple-point Arnoldi methods. AIAA Paper 2003-0616, 2003.
K. Willcox and A. Megretski. Fourier Series for Accurate, Stable, Reduced-Order Models for Linear CFD Applications. SIAM J. Scientific Computing, 26:3, 944–962 (2004).
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© 2005 Springer-Verlag Berlin Heidelberg
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Willcox, K., Lassaux, G. (2005). Model Reduction of an Actively Controlled Supersonic Diffuser. In: Benner, P., Sorensen, D.C., Mehrmann, V. (eds) Dimension Reduction of Large-Scale Systems. Lecture Notes in Computational Science and Engineering, vol 45. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-27909-1_20
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DOI: https://doi.org/10.1007/3-540-27909-1_20
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-24545-2
Online ISBN: 978-3-540-27909-9
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