@inproceedings{oai:jaxa.repo.nii.ac.jp:00006642,
 author = {近藤, 夏樹 and 青山, 剛史 and 齊藤, 茂 and Kondo, Natsuki and Aoyama, Takashi and Saito, Shigeru},
 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 = {This paper presents rotor aerodynamic analysis including influence of a fuselage using an unsteady Euler code. A moving overlapped grid method is applied in the code and four types of grid, inner and outer background grids, blade grid, and fuselage grid are used to accurately simulate the rotor-fuselage interaction. As a result, the effect of the fuselage on rotor aerodynamics is captured in hover and low-speed forward flight conditions by comparing the blade surface pressure with and without the fuselage., 資料番号: AA0047427041, レポート番号: JAXA-SP-03-002},
 pages = {232--237},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {重合格子法を用いたロータ／胴体干渉の計算},
 volume = {JAXA-SP-03-002},
 year = {2004}
}