@inproceedings{oai:jaxa.repo.nii.ac.jp:00006203,
 author = {Yoon, D. H. and 鈴木, 和幸 and 遠藤, 秀之 and 小濱, 泰昭 and Yoon, D. H. and Suzuki, Kazuyuki and Endo, Hideyuki and Kohama, Yasuaki},
 book = {宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第35回・第36回, JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition},
 month = {Feb},
 note = {Aerodynamic performance improvement of the Aero-Train has been conducted both experimentally and numerically. Suction side of the WIG aerofoil tend to separate, because of the existence of the ground surface, and also wing-wing, wing-fuselage interactions appears. Those flow separations limit the lift to drag ratio performance. In order to improve overall Aero-Train performance, optimum wing configuration determination, blowing from the pressure side, and swept forward guide wing configuration are studied., 資料番号: AA0049208021, レポート番号: JAXA-SP-05-012},
 pages = {67--68},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {地面効果翼機の性能向上に関する研究},
 volume = {JAXA-SP-05-012},
 year = {2006}
}