Adaptive Multifidelity Constraints Method for Efficient Multidisciplinary Missile Design Framework

Nhu Van Nguyen, Maxim Tyan, Sunghyun Jin, Jae-Woo Lee
  • Journal of Spacecraft and Rockets, January 2016, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/1.a33312
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The following have contributed to this page: Nhu van Nguyen and Maxim Tyan

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