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Multidisciplinary design optimization of long-range slender guided rockets considering aeroelasticity and subsidiary loads

  • Published:2019-09 Issue: Volume:92 Page:790-805
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Wei Zhao,Long Teng,Shi Renhe,Tang Yifan,Li Huaijian

Funder

National Natural Science Foundation of China

Aeronautic Science Foundation of China

Beijing Institute of Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Guided Weapon Danger Area & Safety Template Generation – A New Capability;Wilson,2008

2. Multi-objective optimization of the aerodynamic shape of a long-range guided rocket;Cao;Struct. Multidisp. Optim.,2018

3. Long-range guided rocket development status and key technology;Chen;Aerodyn. Missile J.,2016

4. System Analysis of High Speed, Long Range Weapon Systems;Moerel,2005

5. Trajectory Simulation of Flexible Missiles and the Effect of Flexibility on Hit Precision;Yao,2014
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