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Interactive, Secure Web-enabled Aircraft Engine Simulation Using XML Databinding IntegrationThis paper discusses the detailed design of an XML databinding framework for aircraft engine simulation. The framework provides an object interface to access and use engine data. while at the same time preserving the meaning of the original data. The Language independent representation of engine component data enables users to move around XML data using HTTP through disparate networks. The application of this framework is demonstrated via a web-based turbofan propulsion system simulation using the World Wide Web (WWW). A Java Servlet based web component architecture is used for rendering XML engine data into HTML format and dealing with input events from the user, which allows users to interact with simulation data from a web browser. The simulation data can also be saved to a local disk for archiving or to restart the simulation at a later time.
Document ID
20040015203
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Lin, Risheng
(Toledo Univ. OH, United States)
Afjeh, Abdollah A.
(Toledo Univ. OH, United States)
Date Acquired
September 7, 2013
Publication Date
October 30, 2003
Publication Information
Publication: Development of a Dynamically Configurable, Object-Oriented Framework for Distributed, Multi-modal Computational Aerospace Systems Simulation
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA Paper 2002-4058
Report Number: AIAA Paper 2002-4058
Meeting Information
Meeting: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAG1-2244
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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