Rapid Geometry Creation for Computer-Aided Engineering Parametric Analyses: A Case Study Using ComGeom2 for Launch Abort System DesignComGeom2, a tool developed to generate Common Geometry representation for multidisciplinary analysis, has been used to create a large set of geometries for use in a design study requiring analysis by two computational codes. This paper describes the process used to generate the large number of configurations and suggests ways to further automate the process and make it more efficient for future studies. The design geometry for this study is the launch abort system of the NASA Crew Launch Vehicle.
Document ID
20070017954
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Hawke, Veronica (Eloret Corp. Sunnyvale, CA, United States)
Gage, Peter (Eloret Corp. Sunnyvale, CA, United States)
Manning, Ted (Eloret Corp. Sunnyvale, CA, United States)
Date Acquired
August 23, 2013
Publication Date
January 11, 2007
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA 2007-0970Report Number: AIAA 2007-0970
Meeting Information
Meeting: 45th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2007
End Date: January 11, 2007
Sponsors: American Inst. of Aeronautics and Astronautics