@techreport{oai:jaxa.repo.nii.ac.jp:00044140,
 author = {山本, 行光 and 渡辺, 光則 and 野村, 茂昭 and 小山, 忠勇 and 穂積, 弘一 and 吉沢, 昭 and 伊藤, 哲一 and 高塚, 均 and YAMAMOTO, Yukimitsu and WATANABE, Mitsunori and NOMURA, Shigeaki and KOYAMA, Tadao and HOZUMI, Koichi and YOSHIZAWA, Akira and ITO, Tetsuichi and TAKATSUKA, HITOSHI},
 month = {Nov},
 note = {Oil flow visualization tests have been made to examine various fore-and afterbody flow patterns on a series of capsule-type vehicles at a Mach number of 7.1 and at angles of attack from 10 to 20 deg. To investigate the effect of the Reynolds number, it was varied from 4.5×104 to 1.8×105 based on aunit length (cm). Model configurationsare classified into two types: blunt cone (S-type) and capsule (M-type). Oilflow photographs indicate that several S-type models show bubble type separations just downstream of the nose-cone juncture region at an angle of attack of α=20゜. However, no separations occur at an angle of α=10゜. Contrary to the results for the S-type, M-type models reveal complex flow separation patterns on the afterbody surface, which depend on model shapes, angles of attack and Reynolds numbers. In this report, these oil flow patterns are analyzed in detail by using topological rules., 資料番号: NALTM0557000, レポート番号: NAL TM-557},
 title = {カプセル型回収体の極超音速オイル・フロウ試験},
 year = {1986}
}