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アイテム

  1. コンテンツタイプ
  2. テクニカルレポート (Technical Report)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 航空宇宙技術研究所(National Aeronautical Laboratory: NAL)
  4. NAL-SP

世界の数値流体力学研究の動向

https://jaxa.repo.nii.ac.jp/records/43119
https://jaxa.repo.nii.ac.jp/records/43119
b01c08de-789e-4169-8315-39662d1b3514
名前 / ファイル ライセンス アクション
nalsp0001001.pdf nalsp0001001.pdf (583.1 kB)
Item type テクニカルレポート / Technical Report(1)
公開日 2015-03-26
タイトル
タイトル 世界の数値流体力学研究の動向
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_18gh
資源タイプ technical report
その他のタイトル(英)
その他のタイトル Progress of Computational Fluid Dynamics in the World
著者 大島, 耕一

× 大島, 耕一

大島, 耕一

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Oshima, Koichi

× Oshima, Koichi

en Oshima, Koichi

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著者所属
宇宙科学研究所
出版者
出版者 航空宇宙技術研究所
出版者(英)
出版者 National Aerospace Laboratory(NAL)
書誌情報 航空宇宙技術研究所特別資料
en : Special Publication of National Aerospace Laboratory SP-1

巻 1, p. 1-6, 発行日 1983-11
抄録(英)
内容記述タイプ Other
内容記述 Firstly, a thermal design method of spacecraft using thermal nodal analysis is briefly reviewed. In this method thermal nodal points are assigned to several representative points of the spacecraft and the thermal balance equations for each nodal point are simultaneously solved. The thermal conductance between the nodal points is corrected using the physical simulation data and the flight data. This may serve as an example in which numerical analysis of the total system can completely replace the physical simulation using large space simulation chambers. Secondly, a vortex method in computational fluid dynamics, re-classified as a mathematical model, is described. In this method the conservation equation of vorticity fixed to the fluid mass elements serves as the basic equation. It has no direct connection with Navier-Stokes equations. The creation of the vorticity is phenomenologically modelled, and the decay is taken into account through numerical dissipation and/or decay of the viscous core. The usefulness of this concept is demonstrated by the unsteady flow field around a rotating elliptic cylinder simulated by this method, which could predict the existence of wake oscillation unrelated to the body oscillation. This existence was confirmed experi-mentally later. Thirdly, the self-similarity of flow fields is discussed, and the concepts of the first and second kinds of self-similarity and of the intermediate asymptotes are introduced. All numerical analysists of fluid dynamic problems should be very careful of the dynamical similarity of the problem which may be involved. Finally, some words are given on the international Conference on Numerical Methods in Fluid Dynamics, which has been playing an internationally important role in information exchange of computational fluid dynamics.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0289-260X
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AN10097345
資料番号
内容記述タイプ Other
内容記述 資料番号: NALSP0001001
レポート番号
内容記述タイプ Other
内容記述 レポート番号: NAL SP-1
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