セラミックタイルのふく射熱伝導連成解析

• 中村 俊哉

  独立行政法人航空宇宙技術研究所

• 甲斐 高志

  独立行政法人航空宇宙技術研究所

書誌事項

タイトル別名

• Combined Radiation-Conduction Analysis of Fibrous Ceramic Tile Insulation
• セラミックタイルの輻射熱伝導連成解析
• セラミックタイル ノ フクシャ ネツ デンドウレンセイカイセキ

抄録

The radiative heat transfer is a dominant heat transfer mechanism at high temperature in the insulation materials of the thermal protection system (TPS) of reentry vehicles because of the high porosity of the materials. It has been well known that serious problems come out when a simple heat conductive analysis is conducted with a thermal conductivity measured by a usual static method and that one should take into account the coupling of radiative and conductive heat transfer in the thermal analysis of such insulations. A finite element code for the combined radiation-conduction analysis is developed. A series of experiments with ceramic tile insulator is also conducted to obtain the fundamental radiative heat transfer properties and to examine the validity of the developed FE program.

収録刊行物

• 日本航空宇宙学会論文集

  日本航空宇宙学会論文集 51 (598), 641-646, 2003

  一般社団法人 日本航空宇宙学会

キーワード

• Heat Transfer
• Radiative Transfer
• Insulation
• Thermal Protection System
• Reentry Vehicle

詳細情報

• CRID: 1390001204470792832
• NII論文ID: 10012565846
• NII書誌ID: AA11307372
• DOI: 10.2322/jjsass.51.641
• ISSN: 24323691
• ISSN: 13446460
• NDL書誌ID: 6767573
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I6767573
• Web Site: https://www.jstage.jst.go.jp/article/jjsass/51/598/51_598_641/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可