A Fast Influence Coefficient Method for Linearized Flutter and Forced-Response Analysis-Reference-Cited by-同舟云学术

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A Fast Influence Coefficient Method for Linearized Flutter and Forced-Response Analysis

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Hsu Kwen¹,Hoyniak Daniel¹

Affiliation:

1. Rolls-Royce Group plc

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-229

Reference14 articles.

1. AGARDManualonAeroelasticityinAxial-FlowTurbomachines,Volumes1and2,AGARD-AG-298,March1987.

2. A Linearized Euler Analysis of Unsteady Transonic Flows in Turbomachinery

3. Predicting Bladerow Interactions Using a Multistage Time-Linearized Navier-Stokes Solver

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