Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions

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dc.contributor.authorBurtsev, B.N.
dc.contributor.authorRyabov, V.I.
dc.contributor.authorSelemenev, S.V.
dc.date.accessioned2016-06-29T15:32:10Z
dc.date.available2016-06-29T15:32:10Z
dc.date.issued2007
dc.identifier.urihttp://hdl.handle.net/20.500.11881/221
dc.language.isoen
dc.subject.otherAerodynamics
dc.titleMathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions

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