Prediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods
Prediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods
| dc.contributor.author | Sibilski, K. | |
| dc.date.accessioned | 2016-06-30T11:50:01Z | |
| dc.date.available | 2016-06-30T11:50:01Z | |
| dc.date.issued | 2000 | |
| dc.identifier.other | 22_13 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/479 | |
| dc.language.iso | en | |
| dc.subject.other | Rotorcraft design | |
| dc.title | Prediction of critical configurations of helicopter - external slung load system using bifurcation theory and continuation methods |
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