Aerodynamic design optimization of helicopter rotor blades in hover performance using advanced configuration generation method

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dc.contributor.authorVu, N.A.
dc.contributor.authorKang, H.J.
dc.contributor.authorAzamatov, A.I.
dc.contributor.authorLee, J.W.
dc.contributor.authorByun, Y.H.
dc.date.accessioned2016-06-29T14:39:20Z
dc.date.available2016-06-29T14:39:20Z
dc.date.issued2009
dc.identifier.otherERF;2009-101177
dc.identifier.urihttp://hdl.handle.net/20.500.11881/102
dc.language.isoen
dc.subject.otherAircraft Design
dc.titleAerodynamic design optimization of helicopter rotor blades in hover performance using advanced configuration generation method

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