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TECHNICAL PAPERS

Development of XML Databinding Integration for Web-Enabled Aircraft Engine Simulation

[+] Author and Article Information
Risheng Lin, Abdollah A. Afjeh

Mechanical, Industrial, and Manufacturing, Engineering Department, The University of Toledo, 2801 West Bancroft Street, Toledo, Ohio 43606

J. Comput. Inf. Sci. Eng 4(3), 186-196 (Sep 07, 2004) (11 pages) doi:10.1115/1.1736686 History: Received April 01, 2003; Revised March 01, 2004; Online September 07, 2004
Copyright © 2004 by ASME
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References

Figures

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Set engine component (Nozzle) operational characteristics
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Engine simulation system control and graphic display output parameters
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Engine simulation configuration file specified in XML file format
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Nozzle simulation data displayed within a user’s web browser
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(a) Decomposition of engine component; (b) Hierarchical engine data object model; (c) Subchildren objects inside nozzle data object
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Engine databinding framework
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Engine schema representation of Nozzle and TransientControl data object model
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Nozzle data class generated by schema compiler process
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Web-based simulation architecture in X-Jgts
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XML-based Java Gas Turbine Simulator accessed from a Web browser
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Engine schematic layout dialog for a simulation model construction

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