@techreport{oai:jaxa.repo.nii.ac.jp:00045072,
 author = {白水, 正男 and 曽我, 国男 and 柴藤, 羊二 and 秋元, 敏男 and SHIROUZU, Masao and SOGA, Kunio and SHIBATO, Yoji and AKIMOTO, Toshio},
 month = {May},
 note = {The normal force on the tail-fins induced by aerodynamic load on front-fins was studied. The magnitude of the induced normal force was obtained experimentally from a wind tunnel test of two-stage rocket models with both front- and tail-fin, with either front- or tail-fin, and without any fin. The test was performed at M∞ = 0.5 ～ 0.95 and 1.5～2.5, and the induced normal force in this region was about 30％, at maximum, of the normal force which acts on the entire model. The variation of the induced normal force with bank angle difference between front- and tail-fin was also obtained from wind tunnel tests of a roll-controllable rocket model at M∞ = 0.50 ～ 1.20. Those results were compared with predictions based on the strip theory. This simplified theory succeeded in giving approximate magnitude and Mach number dependence of the induced normal force ; however, it is not sufficient for precise prediction., 資料番号: NALTR0814000, レポート番号: NAL TR-814},
 title = {小型二段式ロケットの前後翼間の空力干渉による垂直力について},
 year = {1984}
}