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Hypersonic Aeroelastic Stability Boundary Computations Using Radial Basis Functions for Mesh Deformation
dc.contributor.authorLamorte, Nicolasen_US
dc.contributor.authorFriedmann, Peretzen_US
dc.date.accessioned2013-04-08T19:59:45Z
dc.date.available2013-04-08T19:59:45Z
dc.date.issued2012en_US
dc.identifier.citationNicolas Lamorte, Peretz Friedmann, "Hypersonic Aeroelastic Stability Boundary Computations Using Radial Basis Functions for Mesh Deformation", 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 2012, 10.2514/6.2012-5943 <http://hdl.handle.net/2027.42/97135>en_US
dc.identifier.otherAIAA 2012-5943en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/97135
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.titleHypersonic Aeroelastic Stability Boundary Computations Using Radial Basis Functions for Mesh Deformationen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/97135/1/AIAA2012-5943.pdf
dc.identifier.doi10.2514/6.2012-5943en_US
dc.identifier.source18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conferenceen_US
dc.owningcollnameAerospace Engineering, Department of


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