カプセル型回収体の極超音速オイル・フロウ試験

Material type: 文書・図像類

Author: 山本, 行光ほか

Publisher: 航空宇宙技術研究所

Publication date: 1986-11

Material Format: Digital

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Note (General)：: 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 ...

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Material Type: 文書・図像類
Title: カプセル型回収体の極超音速オイル・フロウ試験
Author/Editor: 山本, 行光
渡辺, 光則
野村, 茂昭
小山, 忠勇
穂積, 弘一
吉沢, 昭
伊藤, 哲一
高塚, 均
YAMAMOTO, Yukimitsu
WATANABE, Mitsunori
NOMURA, Shigeaki
KOYAMA, Tadao
HOZUMI, Koichi
YOSHIZAWA, Akira
ITO, Tetsuichi
TAKATSUKA, HITOSHI
Author Heading: 山本, 行光
渡辺, 光則
野村, 茂昭
小山, 忠勇
穂積, 弘一
吉沢, 昭
伊藤, 哲一
高塚, 均
YAMAMOTO, Yukimitsu
WATANABE, Mitsunori
NOMURA, Shigeaki
KOYAMA, Tadao
HOZUMI, Koichi
YOSHIZAWA, Akira
ITO, Tetsuichi
TAKATSUKA, HITOSHI
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1986-11
Publication Date (W3CDTF): 1986-11
Alternative Title: Oil Flow Patterns on a Series of Capsule-Type Re-Entry Vehicles at Hypersonic Speeds
Periodical title: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
No. or year of volume/issue: 557
Volume: 557
Pages: 48-
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: jpn
Target Audience: 一般
Note (General): 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
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44140&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44140&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ