Multidisciplinary aerodynamic/structural design optimization for high subsonic transport wing using approximation technique

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 27, Issue 5, 2006, Pages 810-815

  Zhang, Ke Shi ^a   Han, Zhong Hua ^a   Li, Wei Ji ^a   Li, Xiang ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Aircraft design; High subsonic transport; Kriging model; Multidisciplinary design optimization; Neural networks; Response surface method; Wing

Indexed keywords

AERODYNAMICS; AEROSPACE APPLICATIONS; AIRCRAFT; APPROXIMATION THEORY; DESIGN; ERROR ANALYSIS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NEURAL NETWORKS; NUMERICAL ANALYSIS; OPTIMIZATION; STRAIN; STRESSES; STRUCTURAL ANALYSIS; TRANSONIC FLOW; VISCOUS FLOW;

AIRCRAFT DESIGN; HIGH SUBSONIC TRANSPORT; KRIGING MODEL; MULTIDISCIPLINARY DESIGN OPTIMIZATION; RESPONSE SURFACE METHOD;

WINGS;

EID: 33846155302     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (9)

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