A computational aeroelastic framework based on high-order structural models and high-fidelity aerodynamics
A computational framework for high-fidelity static aeroelastic analysis is presented. Aeroelastic analysis traditionally employs a beam stick representation for the structure and potential, inviscid and irrotational flow assumptions for the aerodynamics. The unique contribution of this work is the i...
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Published in | Aerospace science and technology Vol. 132; p. 108069 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Masson SAS
01.01.2023
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Subjects | |
Online Access | Get full text |
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