국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Low-Speed Wind Tunnel Study of the Direct Lift and Direct Side-Force Characteristics of a Joined-Wing Airplane
저자	Toshimi FUJITA, Akhito IWASAKI, Hirotoshi FUJIEDA, NAOTO TAKIZAWA
Keyword	Low-speed wind tunnel; Joined-wing airplane; Direct Lift; Side-force
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01142.pdf?id=NALTR0001142
보고서번호	NAL TR-1142
발행년도	1992.3
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	Low-speed wind tunnel tests were conducted to obtain aerodynamic data for evaluating direct lift and direct side-force characteristics of four joined-wing airplane models employing a front and rear wing which form diamond shapes in the plan and front view.Tical tail height and body.Resultant direct lift and direct side-force characteristics are presented with respect to the wing area rations (rear/front wing),and include the effect of different control surface area rations and the angle of the control surface.