@inproceedings{oai:jaxa.repo.nii.ac.jp:00005538,
 author = {松崎, 隆久 and 吉岡, 修哉 and 加藤, 琢真 and 小濱, 泰昭 and Matsuzaki, Takahisa and Yoshioka, Shuya and Kato, Takuma 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40回, JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition},
 month = {Feb},
 note = {In spite of the great deal of effort has been made on researching the ground effect in the steady condition, little attention has been given to the ground effect in the unsteady condition. This paper is, therefore, intended as an investigation of the force generated and the flow around the wing when it undergoes unsteady movement at constant speed near the ground. And then it was proven that unsteady aerodynamic characteristics exist in the ground effect when moving in the direction of the height. The cause of these unsteady phenomena was the influence of the induced velocity. The induced velocity is derived from the starting vortex keeping on generating because the circulation around the wing continuously carried on changing when moving heightwise near the ground., 資料番号: AA0063908017, レポート番号: JAXA-SP-07-026E},
 pages = {53--56},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Unsteady aerodynamic characteristics of wings in ground effect},
 volume = {JAXA-SP-07-026E},
 year = {2008}
}