C102 極超音速流の可視化法:放電法(第2報、極超音速流線の可視化)

• 西尾 正富

  福山大学・機械工学

• 真鍋 圭司

  福山大学・機械工学

• 小竹 睦夫

  防衛大学校・航空宇宙工学

抄録

To analyze the flow field around models it is very important to understand the streamlines around the models. However, it has been almost impossible to visualize such streamlines around hypersonic models. Because, the hypersonic flow obtained in laboratory is, in general, very high speed, low density, and short duration. However, methods for visualizing hypersonic streamlines under these experimental conditions have been developed by using the electrical discharge. The principle of the method and visualized hypersonic streamline are demonstrated in this paper.

収録刊行物

• 可視化情報学会誌

  可視化情報学会誌 26 (Supplement2), 123-124, 2006

  社団法人 可視化情報学会

詳細情報

• CRID: 1390282679595004288
• NII論文ID: 10018247298
• NII書誌ID: AA11907562
• DOI: 10.3154/jvs.26.supplement2_123
• 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