B212 極超音速スペースプレーン周り流れ場の可視化およびCFD解析

• 真鍋 圭司

  福山大学

• 中村 弘明

  福山大学

• 西尾 正富

  福山大学

書誌事項

タイトル別名

• Visualization and CFD Analysis around Hypersonic Space Plane

抄録

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

• 可視化情報学会誌

  可視化情報学会誌 26 (Supplement2), 261-262, 2006

  社団法人 可視化情報学会

キーワード

• Space plane
• Electrical Discharge Method
• Finite Element Method

詳細情報

• CRID: 1390001204620806272
• NII論文ID: 10018247536
• NII論文ID: 130003650453
• NII書誌ID: AA11907562
• DOI: 10.3154/jvs.26.supplement2_261
• ISSN: 1884037X
• ISSN: 09164731
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可