Minimum Drag Configurations in Hypersonic Flow Via the Method of Steepest Descent

Authors

  • V. B. Tawakley Defence Science Labortary, Delhi

DOI:

https://doi.org/10.14429/dsj.29.6468

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.

Author Biography

V. B. Tawakley, Defence Science Labortary, Delhi

Defence Science Labortary, Delhi-110 054

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Published

2014-02-24

How to Cite

Tawakley, V. B. (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

Vol. 29 No. 2

Section

General Papers

License

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