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Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach

dc.contributor.authorMader, Charlesen_US
dc.contributor.authorMartins, Joaquimen_US
dc.date.accessioned2012-04-05T20:35:43Z
dc.date.available2012-04-05T20:35:43Z
dc.date.issued2011en_US
dc.identifier.citationMader, Charles; Martins, Joaquim (2011). "Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach." AIAA Journal, vol. 49 no. 12 (2737-2750). <http://hdl.handle.net/2027.42/90642>en_US
dc.identifier.issn0001-1452en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/90642
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleComputation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approachen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationotherUniversity of Toronto; University of Michiganen_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/90642/1/AIAA-55678-904.pdf
dc.identifier.doi10.2514/1.55678en_US
dc.identifier.sourceAIAA Journalen_US
dc.owningcollnameAerospace Engineering, Department of


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