特集Ⅱ 第32回「電磁力関連のダイナミクス」シンポジウム その3
炭素繊維複合材およびドライクロスの誘導加熱解析
2021 年 29 巻 3 号 p. 576-582
詳細
2021 年 29 巻 3 号 p. 576-582
Heating analysis of CFRP and carbon fiber dry cloth for aircraft structures, which is expected for a medium-sized aircraft, is performed. Comparing the temperature of test pieces between numerical and experimental results, validity of both experimental and analytical methods is confirmed for both aluminum and carbon dry cloth sheet. Analysis is made for the layers of carbon dry cloth sheet and CFRTP plate.
