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lan li yan jiu zhong xin zheng zai she ji ren yuan fa she xi tong
Author(s): 
Pages: 63-65
Year: Issue:  2
Journal: Aerospace Control

Keyword:  兰利发射系统研究中心全尺寸模型最佳设计飞行性能飞行特性空间系统人为因素升降副翼;
Abstract: <正> 兰利研究中心已改进其人员发射系统H-20设计的空气动力学性能,以提高其操纵品质和横向飞行性能,同时开始利用H-20的全尺寸模型着手人为因素的研究. 兰利空间系统主管M Pilond说:“我们认为H-20正在接近一种最佳设计.”在过去两年间,研究人员不断努力提高H-20的升/阻比(L/D),致力于改进HL-20的飞行特性和操纵性能.
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