Aerodynamic design optimization of helicopter rotor blades in hover performance using advanced configuration generation method
Aerodynamic design optimization of helicopter rotor blades in hover performance using advanced configuration generation method
| dc.contributor.author | Vu, N.A. | |
| dc.contributor.author | Kang, H.J. | |
| dc.contributor.author | Azamatov, A.I. | |
| dc.contributor.author | Lee, J.W. | |
| dc.contributor.author | Byun, Y.H. | |
| dc.date.accessioned | 2016-06-29T14:39:20Z | |
| dc.date.available | 2016-06-29T14:39:20Z | |
| dc.date.issued | 2009 | |
| dc.identifier.other | ERF;2009-101177 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/102 | |
| dc.language.iso | en | |
| dc.subject.other | Aircraft Design | |
| dc.title | Aerodynamic design optimization of helicopter rotor blades in hover performance using advanced configuration generation method |
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