@inproceedings{oai:jaxa.repo.nii.ac.jp:00005772,
 author = {磯貝, 紘二 and Isogai, Koji},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)},
 month = {Mar},
 note = {SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20000117-20000119 東京 日本, SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20000117-20000119 Tokyo Japan, A computer code for aeroelastic tailoring of an arrow wing supersonic cruise configuration is developed. A direct search method is employed to find the optimum fiber orientation angles and thickness distributions of the upper and lower skin panels of the wing box for the minimum weight design under the multiple constraints. The static strength, symmetric and antisymmetric flutter velocities are taken into account at the same time as the constraints. The code is applied to a typical arrow wing configuration to demonstrate its capabilities., 資料番号: AA0063609041, レポート番号: JAXA-SP-06-029E},
 pages = {353--359},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Application of direct search method to aeroelastic tailoring of an arrow wing configuration},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}