국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Experimental Studies of Vortex Flaps and Vortex Plates Part 2 1.15 m Span 60°Delta Wing
저자	Kenichi RINOIE John L. STOLLERY
Keyword	low-speed aerodynamics; delta wing; vortex flap; leading-edge separation vortex
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr1180t.pdf?id=NALTR0001180T
보고서번호	NAL TR-1180T
발행년도	1992.10
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	Low-speed wind tunnel tests were carried out on several vortex flap and vortex plate configuration to assess their benefits.The force and surface pressure measurements were taken using gher than the stall incidence.The performance of a vortex plate protruding from the leading-edge of the datum delta wing is shown to be comparable to that of the vortex flap.However,when the vortex plate is used with the vortex flap deflected,these tests showed no benefits.