@techreport{oai:jaxa.repo.nii.ac.jp:00043804,
 author = {高島, 一明 and 谷, 喬 and 関根, 英夫 and 中村, 正剛 and TAKASHIMA, Kazuaki and TANI, Takashi and SEKINE, Hideo and NAKAMURA, Seigo},
 month = {May},
 note = {Longitudinal dynamic stability derivatives of NAL-7 rocket models of different body  length are measured by a longitudinal dynamic test and a roll dynamic test with angles of   attack in wind tunnels at M=0.  6・2. 0 and by free  flight test. Both the results of wind  tunnels and of free flight test are compard, and they show fairly good agreement.  Another rocket configuration models are also tested in wind tunnels at M=0.6,--3.0.     Roll damping derivatives of these models are measured at the same Mach number range.  Some of these results show the interaction of wing to wing at subsonic and low super- sonic ranges. At the range of M 1.2, the experimental data agree precisely with the  calculated values., 資料番号: NALTM0221000, レポート番号: NAL TM-221},
 title = {ロケット模型の動安定微係数の測定},
 year = {1972}
}