An adjoint-based optimization method for helicopter fuselage backdoor geometry

dc.contributor.author Zhang, Q.
dc.contributor.author Lee, J.-D.
dc.contributor.author Wendisch, J.-H.
dc.date.accessioned 2016-07-01T13:10:07Z
dc.date.available 2016-07-01T13:10:07Z
dc.date.issued 2010
dc.identifier.other Q.ZHANG_123_paper
dc.identifier.uri http://hdl.handle.net/20.500.11881/956
dc.language.iso en
dc.subject.other Numerical Methods
dc.title An adjoint-based optimization method for helicopter fuselage backdoor geometry
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