Visualization of Supersonic Flow Using Computer Image Processing Technique.

• HASHIMOTO Masayuki

  (株)村田製作所 野洲事業所

• SHIZAWA Takaaki

  東京理科大学工学部

• HONAMI Shinji

  東京理科大学工学部

• MURAKAMI Akira

  航空宇宙技術研究所

• SHINDO Shigemi

  航空宇宙技術研究所

• SAKATA Kimio

  航空宇宙技術研究所

Bibliographic Information

Other Title

• 画像処理による超音速流れの可視化解析
• ガゾウ ショリ ニ ヨル チョウオンソク ナガレ ノ カシカ カイセキ

Abstract

This paper presents a flow visualization study of swept shock wave / turbulent boundary layer interactions using computer image processing technique in the supersonic flow at Mach number of 3.1. The test model is composed of a flat plate and sharp fins. Images obtained from oil-spot, liquid crystal coatings for surface shear force and vapor screen visualization were processed. Streaklines of oil spots are determined quantitatively by an active threshold selection method. By image processes of liquid crystal coatings for surface shear force and vapor screen, the spatial relation among shear stress distribution, separation lines and separation vortex is clarified. Surface pressure distribution is integrated into these processed images for comparison.

Journal

• Journal of the Visualization Society of Japan

  Journal of the Visualization Society of Japan 19 (73), 141-146, 1999

  The Visualization Society of Japan

Keywords

• Supersonic Flow
• Flow Visualization
• Integration of Visual Information

Details

• CRID: 1390001204618479744
• NII Article ID: 10002003998
• NII Book ID: AN10374478
• DOI: 10.3154/jvs.19.73_141
• ISSN: 1884037X
• ISSN: 09164731
• NDL BIB ID: 4688404
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I4688404
• Text Lang: ja
• Data Source:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• Abstract License Flag: Disallowed