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    Ramjet Powered Missile Design Using a Genetic Algorithm

    Source: Journal of Computing and Information Science in Engineering:;2007:;volume( 007 ):;issue: 002::page 167
    Author:
    Roy J. Hartfield
    ,
    Rhonald M. Jenkins
    ,
    John E. Burkhalter
    DOI: 10.1115/1.2738722
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A 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.
    keyword(s): Design , Missiles , Ramjets , Shock (Mechanics) , Genetic algorithms AND Modeling ,
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      Ramjet Powered Missile Design Using a Genetic Algorithm

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    http://yetl.yabesh.ir/yetl1/handle/yetl/135388
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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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    DSpace software copyright © 2002-2015  DuraSpace
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