@inproceedings{oai:jaxa.repo.nii.ac.jp:00006527,
 author = {神田, 淳 and 甲斐, 高志 and 中村, 俊哉 and Kanda, Atsushi and Kai, Takashi and Nakamura, Toshiya},
 book = {宇宙航空研究開発機構特別資料: 第69回風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 69th Meeting},
 month = {Feb},
 note = {For the anti-symmetric flutter speeds of a tip-fin-shaped reentry space vehicle model, numerical predictions using Doublet-Point Method (DPM) have been different from experimental results in a part of lower supersonic region. The cause of the discrepancy is suspected to be that the local flow over the wing differs from the free stream. Instead of free stream Mach numbers, measured local Mach numbers are adopted for flutter boundary analyses, and the corrected numerical results show good agreement with experimental ones. Therefore, it is made clear that the correction by local Mach numbers improves the accuracy of the flutter boundary., 資料番号: AA0048061002, レポート番号: JAXA-SP-04-008},
 pages = {8--12},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {計測局所マッハ数による非平面翼のフラッタ限界値補正},
 volume = {JAXA-SP-04-008},
 year = {2005}
}