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  1. コンテンツタイプ
  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

Nonequilibrium Flow around Blunt Body with Thermal Radiation

https://jaxa.repo.nii.ac.jp/records/34524
https://jaxa.repo.nii.ac.jp/records/34524
7455e2e1-db9e-4960-8622-f7d253a10788
名前 / ファイル ライセンス アクション
SA2401259.pdf SA2401259.pdf (2.1 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Nonequilibrium Flow around Blunt Body with Thermal Radiation
言語 en
言語
言語 eng
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
著者 LEE, Jong-Hun

× LEE, Jong-Hun

en LEE, Jong-Hun

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KAWAMURA, Ryuma

× KAWAMURA, Ryuma

en KAWAMURA, Ryuma

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出版者
出版者 東京大学宇宙航空研究所
出版者(英)
出版者 Institute of Space and Aeronautical Science,University of Tokyo
書誌情報 en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

巻 42, 号 1, p. 1-40, 発行日 1977-01
抄録(英)
内容記述タイプ Other
内容記述 Chemical nonequilibrium and radiating flow in the stagnation region of a hypersonic blunt body is investigated in the merged layer regime. The coupling phenomena between nonequilibrium chemical reaction and radiation are studied for a multicomponent air mixture. The radiative energy transfer is simplified to the emission-dominated case. The basic model of the flow is described by the simplified Navier-Stokes equations based on the thin layer assumption. Using the concept of local similarity, the equations are reduced to a set of nonlinear, coupled ordinary differential equations. This set of equations is solved using a new numerical technique called SAR Method. Solutions are obtained for a blunt body flying at 10 km/sec and for a free-stream Reynolds number range of 500 to 5730. The results show that a strong coupling exists between the nonequilibrium chemical reactions and the radiation cooling effects, and that the radiative heat transfer to the body is considerably reduced due to the reaction dominated nature in the combined flow. The physical interpretation of these phenomena and the detailed behaviour of the flowfield are discussed. In order to develop the discussions of results in more general sense, the influence of the body nose radius on the behaviour of the flowfield is also investigated in the present paper.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0372-1418
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00675986
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2401259000
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