@article{oai:toyama.repo.nii.ac.jp:00016440,
 author = {楠瀬, 一洋 and 松島, 紀佐 and 後藤, 悠一郎 and 丸山, 大悟 and 山下, 博 and 米澤, 誠仁},
 issue = {636},
 journal = {日本航空宇宙学会論文集, JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES},
 month = {},
 note = {application/pdf, One of the fundamental problems preventing commercial transport aircraft from supersonic flight is the creation of strong shock waves. Here, a biplane concept is proposed that will enable a significant reduction of shock waves: Introduce a second wing nearly parallel to the conventional wing, creating a biplane configuration. The interaction between the two wings will cancel or reduce the shock waves created by the individual wings. Several simple two-dimensional biplane configurations are currently under study, using CFD (computational fluid dynamics) codes, Euler calculations for inviscid flow analysis and inverse-problem analysis for wing design, to demonstrate our biplane concept., Article, 日本航空宇宙学会論文集=JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 55(636), 1-7.(2007)},
 pages = {1--7},
 title = {衝撃波の相殺効果を利用した複葉超音速翼型の研究},
 volume = {55},
 year = {2007}
}