書誌事項
- タイトル別名
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- Visualization and CFD Analysis around Hypersonic Space Plane
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The flowfield analysis around a model of space plane traveling at Mach 10 has been carried out utilizing an Electrical Discharge Method and a Finite Element Method scheme. In this study, the experiments and the numerical simulations were carried out under the conditions the angle of attack were 0 and 10 deg. Furthermore, the experimental results were compared with the numerical ones. In these comparisons, it was found that they were relatively in good agreement.
収録刊行物
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- 可視化情報学会誌
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可視化情報学会誌 26 (Supplement2), 261-262, 2006
社団法人 可視化情報学会
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詳細情報 詳細情報について
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- CRID
- 1390001204620806272
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- NII論文ID
- 10018247536
- 130003650453
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- NII書誌ID
- AA11907562
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- ISSN
- 1884037X
- 09164731
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可