著者
山名 正夫 伊藤 光
出版者
一般社団法人 日本航空宇宙学会
雑誌
日本航空宇宙学会誌 (ISSN:00214663)
巻号頁・発行日
vol.23, no.255, pp.251-257, 1975-04-05 (Released:2009-05-25)
参考文献数
2

The generation of a kind of circulatory flow in the separated-flow region of a stalled sweptback wing was noticed. Observation on the circulatory flow was made for a model airplane by using evaported-gas-oil smoke. The presence of a strong lateral outward flow was observed in the considerable range behind the trailing edge of wing-root portions. The effect of the angle of sweep back and taper ratio of a wing on the intensity and direction of the circulatory flow were also investigated.