Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computers
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Reuther, J., Alonso, J. J., Rimlinger, M. J., & Jameson, A.
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Reuther, J||Alonso, JJ||Rimlinger, MJ||Jameson, A
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40 Engineering
4001 Aerospace Engineering
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http://dx.doi.org/10.1016/s0045-7930(98)00050-4
