Detection of Boundary-Layer Transition in a Cryogenic Wind Tunnel by Using Luminescent Paint

• ASAI Keisuke

  National Aerospace Laboratory

• KANDA Hiroshi

  National Aerospace Laboratory

• KUNIMASU Tetsuya

  National Aerospace Laboratory

• LIU Tianshu

  Purdue Univ

• SULLIVAN John P.

  Purdue Univ

収録刊行物

• Album of visualization

  Album of visualization 14 13-14, 1997-12

キーワード

• Boundary-layer transition
• temperature sensitive paint
• cryogenic wind tunnel
• Reynolds number effect

詳細情報

• CRID: 1572543023941753472
• NII論文ID: 10002512589
• NII書誌ID: AN10445918
• ISSN: 09194630
• 本文言語コード: en
• データソース種別:
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