@inproceedings{oai:jaxa.repo.nii.ac.jp:00036823,
 author = {航空宇宙技術研究所 and 三菱重工業 and 川崎重工業 and 富士重工業 and National Aerospace Laboratory and Mitsubishi Heavy Industries  Ltd and Kawasaki Heavy Industries  Ltd and Fuji Heavy Industries  Ltd},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {May},
 note = {以下の主題について論じた。オイル流れの可視化、抗力測定、3次元境界層遷移、圧縮性境界層、超音速層流制御、圧縮性層流制御、ファスナー接合要素解析、ファスナー接合構造要素における熱伝導、流体と構造物間の熱伝達、超音速機用軽金属材料、超音速機用繊維/金属ラミネート、耐損傷胴体構造解析、炭素繊維強化プラスチック複合部材の非破壊評価、T字型補強部材の座屈、および補強部材の表皮剥離。, The following topics were discussed: oil flow visualization, drag measurement, three dimensional boundary layer transition, compressible boundary layers, supersonic laminar flow control, compressible laminar flow control, fastener jointed component analysis, heat conduction in fastener jointed structural components, thermal transfer between fluid and structure, light metallic materials for supersonic transport, fiber/metal laminates for supersonic transport, damage tolerant fuselage structure analysis, nondestructive evaluation for carbon fiber reinforced plastic composites member, buckling of T-shaped stiffener, and skin disbond of stiffener., 資料番号: AA0000440000, レポート番号: NAL SP-31},
 pages = {1--168},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {Government-industry specific joint research on the advanced aircraft component technologies, Final report},
 volume = {31},
 year = {1996}
}