1402 ベークライト感温模型による空力加熱測定

• 飯野 真

  東理大院

• 石川 仁

  東理大工

• 中川 宗敬

  JAST

• 津田 大介

  JAXA

• 坂上 博隆

  JAXA

書誌事項

タイトル別名

• 1402 Aerodynamic Heating Measurement Using Bakelite based Temperature Sensor Model

抄録

In recent years, research of space plane and hypersonic airliner has been eagerly studied in the aerospace field, and a technique for measuring the temperature and pressure changes in the airframe surface is essential. Many researchers focus on the Temperature-Sensitive Paint (TSP) and Pressure-Sensitive Paint (PSP) as a technique for measuring them. In this study, we investigate a temperature measurement using Bakelite as visualization measurement method. It was possible to measure the stagnation temperature of the hemisphere model as the temperature distribution image in hypersonic wind tunnel based on the relationship between the temperature and the emission intensity of Bakelite.

収録刊行物

• 流体工学部門講演会講演論文集

  流体工学部門講演会講演論文集 2014 (0), _1402-1_-_1402-2_, 2014

  一般社団法人 日本機械学会

キーワード

• Hypersonic
• Thermal Quenching
• Aerodynamic Heating
• Bakelite

詳細情報

• CRID: 1390001205884539008
• NII論文ID: 110009938779
• DOI: 10.1299/jsmefed.2014._1402-1_
• ISSN: 24242896
• Web Site: https://www.jstage.jst.go.jp/article/jsmefed/2014/0/2014__1402-1_/_pdf
• 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