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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