Robust Aerodynamic Design of Mars Exploratory Airplane Wing with a New Optimization Method

Robust Aerodynamic Design of Mars Exploratory Airplane Wing with a New Optimization Method. Shimoyama, K. Ph.D. Thesis, School of Engineering, The University of Tokyo, Japan, February, 2006.
bibtex

@phdthesis{Shimoyama06,
   author = {Koji Shimoyama},
   title = {Robust {A}erodynamic {D}esign of {M}ars {E}xploratory {A}irplane {W}ing
   with a {N}ew {O}ptimization {M}ethod},
   school = {School of Engineering, The University of Tokyo},
   address = {Japan},
   month = {February},
   year = {2006}
}

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