@article{oai:jaxa.repo.nii.ac.jp:00021730,
 author = {古賀, 星吾 and 互井, 梨絵 and 日高, 亜希子 and 中野, 英一郎 and 永井, 伸治 and Koga, Seigo and Tagai, Rie and Hidaka, Akiko and Nakano, Eiichiro and Nagai, Shinji},
 issue = {5},
 journal = {日本航空宇宙学会論文集, Journal of the Japan Society for Aeronautical and Space Sciences},
 month = {Oct},
 note = {For a design of a reentry capsule and its flight, one of the most important problems is an assessment of the dynamic stability in transonic speed. In this study, dynamic stability tests for a lifting capsule were conducted with the 1-DOF free-rotation test method in the JAXA 2m × 2m Transonic Wind Tunnel. In this test method, the reduced frequency and time history of the angular motion in non-dimensional time could be matched between the wind-tunnel test and the actual flight. Effects of flow conditions, location of center of gravity, an ablated shape, surface roughness and model MOI were discussed with the obtained time-series angular data and schlieren photographs. Furthermore, a new data processing method was developed for calculating the damping coefficients. The obtained amplitude and frequency of the oscillations, and the estimated damping coefficients give helpful information for the project planning., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: DS1640221005},
 pages = {281(29)--287(35)},
 title = {自由回転試験による揚力カプセルの遷音速動特性の考察},
 volume = {64},
 year = {2016}
}