Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions
Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions
| dc.contributor.author | Burtsev, B.N. | |
| dc.contributor.author | Ryabov, V.I. | |
| dc.contributor.author | Selemenev, S.V. | |
| dc.date.accessioned | 2016-06-29T15:32:10Z | |
| dc.date.available | 2016-06-29T15:32:10Z | |
| dc.date.issued | 2007 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/221 | |
| dc.language.iso | en | |
| dc.subject.other | Aerodynamics | |
| dc.title | Mathematical modeling of Ka-226 / Ka-26 helicopter main rotor blade flapping motion at rotor acceleration / deceleration in wind conditions |
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