@techreport{oai:jaxa.repo.nii.ac.jp:00041231,
 author = {楯, 篤志 and 渡辺, 光則 and 野田, 順一 and 関根, 英夫 and 吉永, 崇 and Tate, Atsushi and Watanabe, Mitsunori and Noda, Junichi and Sekine, Hideo and Yoshinaga, Takashi},
 month = {Dec},
 note = {ロケット･ブースターおよびロケット自体の安定的な回収のためのデータを得るためにいくつかのマッハ数の超音速流中で、大迎角(32度以上)の鈍頭円柱に作用する横力の測定が行われた。平面と準楕円形を含む鈍頭円柱が横力へのノーズ部の形態の効果を決定するために試験された。平面の円柱に近い高度に鈍い頭の円柱はマッハ数が減少するにつれてより大きな横力を示し、平面の円柱はマッハ数が1.75と2.25の間の狭い領域で大きな横力を示した。, To obtain data for stable recovery of future rocket boosters and the rocket itself, measurements of side force acting on blunted circular cylinders were carried out at high angles of attack (alpha less than 32 deg.) in supersonic flows of several Mach numbers. The blunted circular heads, including a flat face and semi-elliptic shapes, were tested to determine the effects of nose shapes on side force. Highly blunted bodies close to a flat-faced cylinder show large side force as the Mach number decreases, while a flat-faced cylinder shows large side force in the narrow regions between M(sub infinity) = 1.75 and 2.25., 資料番号: AA0004262000, レポート番号: NAL TR-1255},
 title = {超音速流中の大迎角鈍頭円柱に作用する横力},
 year = {1994}
}