Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing

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Autoria(s): 杨国伟; 陈大伟; 崔凯

Data(s)	2009
Identificador	http://dspace.imech.ac.cn/handle/311007/33545 http://www.irgrid.ac.cn/handle/1471x/8987
Idioma(s)	英语
Fonte	Journal Of Aircraft.2009,46(4):1444-1450
Palavras-Chave	#Navier-Stokes Solver #Aircraft
Tipo	期刊论文