Prediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods

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dc.contributor.authorSibilski, K.
dc.date.accessioned2016-06-30T11:50:01Z
dc.date.available2016-06-30T11:50:01Z
dc.date.issued2000
dc.identifier.other22_13
dc.identifier.urihttp://hdl.handle.net/20.500.11881/479
dc.language.isoen
dc.subject.otherRotorcraft design
dc.titlePrediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods

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