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

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dc.contributor.authorIvtchin, V.A.
dc.contributor.authorTischenko, M.N.
dc.contributor.authorAnimitsa, V.A.
dc.contributor.authorGolovkin, V.A.
dc.date.accessioned2016-08-15T13:51:26Z
dc.date.available2016-08-15T13:51:26Z
dc.date.issued1996
dc.identifier.otherERF-1996-Vol1-15
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3131
dc.language.isoen
dc.titleAnalysis of model and full-scale investigation results of helicopter blade aerodynamic configuration effect on pitch link load

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