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Enhanced Design Process with CAD/CAE Integration and Smart Knowledge Capturing MethodGujarathi, Ganesh Unknown Date
No description available.
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Application of binary space partitioning trees to geometric modeling and ray-tracingThibault, William Charles 12 1900 (has links)
No description available.
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Sterolithography (SL) cure modelingTang, Yanyan 08 1900 (has links)
No description available.
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Application of concurrent engineering methods to the design of an autonomous aerial robotIngalls, Stephen A. 12 1900 (has links)
No description available.
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A decision support system for fabrication process planning in stereolithographyWest, Aaron P. 05 1900 (has links)
No description available.
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A tolerance representation scheme for solid modelsBaum, Robert Adam 05 1900 (has links)
No description available.
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Surface roughness and draft angle effects on stereolithography moldsCedorge, Thomas 05 1900 (has links)
No description available.
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Engineering data integration in a discrete part design and manufacturing environmentRangan, Ravi M. 08 1900 (has links)
No description available.
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Development of digital image analysis and stereological techniques to incorporate microstructural information in finite element based simulationsYang, Shichen 05 1900 (has links)
No description available.
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Knowledge Based Integrated Multidisciplinary Aircraft Conceptual DesignMunjulury, Venkata Raghu Chaitanya January 2014 (has links)
With the ever growing complexity of aircrafts, new tools and eventually methods to use these tools are needed in aircraft conceptual design. To reduce the development cost, an enhancement in the conceptual design is needed. This thesis presents a knowledge-based aircraft geometry design tool RAPID and the methodology applied in realizing the design. The parameters used to create a geometry need to be exchange between different tools. This is achieved by using a centralized database or onedata concept. One-database will enable creating a less number of cross connections between different tools to exchange data with one another. Different types of aircraft configurations can be obtained with less effort. As RAPID is developed based on relational design, any changes made to the geometric model will update automatically. The geometry model is carefully defined to carry over to the preliminary design. The validation of RAPID is done by implementing it in different aircraft design courses at Linköping University. In the aircraft project course, RAPID was effectively used and new features were added to the obtained desired design. Knowledge-base is used to realize the design performance for the geometry with an integrated database approach for a multidisciplinary aircraft conceptual design.
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