@inproceedings{oai:jaxa.repo.nii.ac.jp:00006612,
 author = {藤村, 哲司 and 篠崎, 正治 and Fujimura, Tetsuji and Shinozaki, Masaharu},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {Recently, cutting aero-engine development cycle times is being pursued aggressively to reduce program risk as well as total amount of costs. Under such a back ground with very rapid progress of computer utilization environment, numerical simulations have been extensively applied to aero-engine structural design. From the viewpoint of recent trend of advanced detailed and multidisciplinary design approach, detailed non-linear finite element analysis, rotor dynamics, crack growth analysis and impact analysis are presented., 資料番号: AA0047427011, レポート番号: JAXA-SP-03-002},
 pages = {59--64},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ガスタービン設計における構造解析の現状},
 volume = {JAXA-SP-03-002},
 year = {2004}
}