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contributor authorRoy J. Hartfield
contributor authorRhonald M. Jenkins
contributor authorJohn E. Burkhalter
date accessioned2017-05-09T00:23:03Z
date available2017-05-09T00:23:03Z
date copyrightJune, 2007
date issued2007
identifier issn1530-9827
identifier otherJCISB6-25975#167_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135388
description abstractA methodology for developing optimized designs for symmetric-centerbody ramjet powered missiles, using a genetic algorithm as the driver for the system optimization process, has been developed. The methodology described in this paper allows for a comprehensive but efficient exploration of the design space. This global optimization process is made possible by performance prediction codes, which can provide preliminary design-level accuracy very efficiently. This work demonstrates the first truly comprehensive design strategy for this type of device. The paper contains a discussion of the methodology and shows results for a typical design scenario.
publisherThe American Society of Mechanical Engineers (ASME)
titleRamjet Powered Missile Design Using a Genetic Algorithm
typeJournal Paper
journal volume7
journal issue2
journal titleJournal of Computing and Information Science in Engineering
identifier doi10.1115/1.2738722
journal fristpage167
journal lastpage173
identifier eissn1530-9827
keywordsDesign
keywordsMissiles
keywordsRamjets
keywordsShock (Mechanics)
keywordsGenetic algorithms AND Modeling
treeJournal of Computing and Information Science in Engineering:;2007:;volume( 007 ):;issue: 002
contenttypeFulltext


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