@inproceedings{oai:jaxa.repo.nii.ac.jp:00006148,
 author = {町田, 健太郎 and 宮路, 幸二 and Machida, Kentaro and Miyaji, Koji},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005},
 month = {Feb},
 note = {A 3D flutter of a sweptback wing is numerically investigated by coupling inviscid flow simulations with a bending-torsion beam structure model. The beam model of a 3D wing is a natural extension of a widely used 2D 2-degree-of-freedom structure model and it considerably simplifies the structure analysis. Finite-volume unstructured CFD is used with the aim of applying various configurations in the future. The grid is dynamically deformed in accordance with the wing motion. A truss-analogy is applied to determine the new positions of interior points when the displacements of boundary points are specified. A well-known experiment using the AGARD standard aeroelastic configuration called 445.6 wing is selected for the validation. The developed methods successfully simulated the experimental flutter boundary., 資料番号: AA0049212015, レポート番号: JAXA-SP-05-017},
 pages = {94--99},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {曲げ・捩り梁構造モデルと非構造CFDによる3次元翼フラッタ解析},
 volume = {JAXA-SP-05-017},
 year = {2006}
}