Analysis of model and full-scale investigation results of helicopter blade aerodynamic configuration effect on pitch link load

dc.contributor.author	Ivtchin, V.A.
dc.contributor.author	Tischenko, M.N.
dc.contributor.author	Animitsa, V.A.
dc.contributor.author	Golovkin, V.A.
dc.date.accessioned	2016-08-15T13:51:26Z
dc.date.available	2016-08-15T13:51:26Z
dc.date.issued	1996
dc.identifier.other	ERF-1996-Vol1-15
dc.identifier.uri	http://hdl.handle.net/20.500.11881/3131
dc.language.iso	en
dc.title	Analysis of model and full-scale investigation results of helicopter blade aerodynamic configuration effect on pitch link load

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