기술보고서

기술보고서 게시판 내용
타이틀	Some Effects of Mach Number on the Transonic Flutter Characteristics of Thin Cantilever Wings Having a Taper Ratio 0.6 and a Sweptback Angle of 45°
저자	Eiichi NAKAI, Akira OHARA
Keyword
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr00061.pdf?id=NALTR0000061
보고서번호	NAL TR-61
발행년도	1964.2
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT