A Reduced Order Method for Grid Deformation in Aeroelasticity Analysis-Reference-Cited by-同舟云学术

A Reduced Order Method for Grid Deformation in Aeroelasticity Analysis

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Yang H. Q.¹

Affiliation:

1. CFD Research Corp.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-890

Reference13 articles.

1. Implicit flux-split Euler schemes for unsteady aerodynamic analysis involving unstructured dynamic meshes

2. Dixon, S.C., 1966, "Comparison of Panel Flutter Results fromApproximate Aerodynamic Theory with Results from ExactInviscidTheoryandExperiment,"NASA TND-3649,Oct.1966.

3. Gupta, K.K., 1997, "STRAS - An Integrated, Multidisciplinary, Finite-Element, Structural, Fluids, Aeroelastic, and Aeroservoelastic Analysis Computer Program",NASATechnicalMemorandumNo.4795.

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