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錐体まわりの超音速流に対する近似解
https://jaxa.repo.nii.ac.jp/records/31659
https://jaxa.repo.nii.ac.jp/records/31659c6d57949-8ea4-45ea-a3b5-b87140daeba1
名前 / ファイル | ライセンス | アクション |
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SA0124648.pdf (755.2 kB)
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Item type | 紀要論文 / Departmental Bulletin Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 錐体まわりの超音速流に対する近似解 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | departmental bulletin paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Approximate Solutions to the Supersonic Flow around Conical Bodies | |||||
著者 |
松野, 謙一
× 松野, 謙一× 河村, 龍馬× MATSUNO, Ken-ichi× KAWAMURA, Ryuma |
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著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science University of Tokyo | ||||||
出版者 | ||||||
出版者 | 東京大学宇宙航空研究所 | |||||
書誌情報 |
東京大学宇宙航空研究所報告 巻 12, 号 3, p. 713-735, 発行日 1976-08 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 超音速流中におかれた非軸対称錐体,または,有迎角円錐まわりの流れに対する近似方程式および,その解を提示する。本近似理論は,等エントロピ流仮定に基づく線型理論である.無迎角円錐に対するTaylor-Maccollの厳密解を基本とし,それからの微小擾乱の考えを用いることにより,近似方程式を導出し,その解法を示す.例として,有迎角円錐,及び楕円錐まわりの流れに適用した.他の近似理論,実験結果と比較することにより,その有効性が示された. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An analytical method of solution to the flow over slightly yawed conical body are presented. The cross section of the body is assumed to be nearly circular but otherwise arbitrary. The conical flow equations and boundary conditions are linearized by means of small perturbation from the Taylor-Maccoll conical flow solution for unyawed circular cone. The equations are simplified by the use of isentropic assumption and the solutions are obtained analytically. It is applied to the cases of slightly yawed circular cones and elliptic cones. The results ale compared with experiment and with other approximate solutions. and it is shown that for the circular cones and elliptic cones, the simplest closed form solution based on the density-constant approximation estimates the aerodynamic characteristics fairly well. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0563-8100 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00161914 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA0124648000 |