A new procedure for aerodynamic missile designs using topological optimization approach of continuum structures

Aerospace Science and Technology

Volumn 10, Issue 5, 2006, Pages 364-373

  Luo, Zhen ^a   Yang, Jingzhou ^b   Chen, Liping ^c  

^a CHINESE UNIVERSITY OF HONG KONG   (Hong Kong)

^b UNIVERSITY OF IOWA   (United States)

^c HUAZHONG UNIVERSITY OF SCIENCE AND TECHNOLOGY   (China)

Author keywords

Aerodynamic missiles; Compromise programming; Mathematical programming; Multi objective; Multilevel sequence programming; Structural topology optimization

Indexed keywords

AERODYNAMICS; COMPUTER PROGRAMMING; COMPUTER SOFTWARE; CONTINUUM MECHANICS; EIGENVALUES AND EIGENFUNCTIONS; INTERPOLATION; LOADS (FORCES); MATHEMATICAL PROGRAMMING; OPTIMIZATION; TOPOLOGY;

AERODYNAMIC MISSILES; COMPROMISE PROGRAMMING; MULTI-OBJECTIVE; MULTILEVEL SEQUENCE PROGRAMMING; STRUCTURAL TOPOLOGY OPTIMIZATION;

MISSILES;

EID: 33745654352     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2005.12.006     Document Type: Article

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