2026-03-15T20:10:00Z https://jaxa.repo.nii.ac.jp/oai

oai:jaxa.repo.nii.ac.jp:00045188 2023-06-20T21:43:45Z 1887:1893 1896:1898:1913:1917

Design, construction and performance of a gust generating device for a half model test in the 6.5m×5.5m low speed wind tunnel. 半截模型用突風発生装置の設計製作とその特性 鈴木, 誠三 外立, 政隆 室田, 勝一 萱場, 重男 菊池, 孝男 SUZUKI, Seizo HASHIDATE, Masataka MUROTA, Katsuichi KAYABA, Shigeo KIKUCHI, Takao A gust generating system was constructed for the test of a gust alleviation device conducted in the NAL′s 6.5m×5.5m low speed wind tennel. This system makes use of tip vortices shedding from a pair of cantileved, oscillating wings. The Dryden model of atmospheric turbulence was successfully simulated with this system; and wind tunnel tests for developing a gust load alleviation technique for an energy efficient type of future transport with a high aspect ratio wing were conducted with good results. 資料番号: NALTR0929000 レポート番号: NAL TR-929 航空宇宙技術研究所 National Aerospace Laboratory(NAL) 1987-04 eng technical report https://jaxa.repo.nii.ac.jp/records/45188 0389-4010 航空宇宙技術研究所報告 Technical Report of National Aerospace Laboratory TR-929 929 38 https://jaxa.repo.nii.ac.jp/record/45188/files/naltr00929.pdf application/pdf 2.6 MB 2020-01-29