文章基本信息

标题：Minimum Drag Configurations in Hypersonic Flow Via the Method of Steepest Descent
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作者：V. B. Tawakley
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2014
卷号：29
期号：2
页码：55-62
DOI：10.14429/dsj.29.6468
语种：English
出版社：Defence Scientific Information & Documentation Centre
摘要：It has been shown that the problem of finding minimum drag configuration in hypersonic flow can be reduced to a problem in optimum control and the method of steepest ascent is a useful tool for finding the solution of this problem.
关键词：Hypersonic flow;Optimum control