Minimum Drag Configurations in Hypersonic Flow Via the Method of Steepest Descent
Keywords:
Hypersonic flow, Optimum control
Abstract
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.
Published
2014-02-24
How to Cite
Tawakley, V. (2014). Minimum Drag Configurations in Hypersonic Flow Via the Method of Steepest Descent. Defence Science Journal, 29(2), 55-62. https://doi.org/10.14429/dsj.29.6468
Issue
Section
General Papers
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