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Aircraft Conceptual Design Using Vehicle Sketch PadVehicle Sketch Pad (VSP) is a parametric geometry modeling tool that is intended for use in the conceptual design of aircraft. The intent of this software is to rapidly model aircraft configurations without expending the expertise and time that is typically required for modeling with traditional Computer Aided Design (CAD) packages. VSP accomplishes this by using parametrically defined components, such as a wing that is defined by span, area, sweep, taper ratio, thickness to cord, and so on. During this phase of frequent design builds, changes to the model can be rapidly visualized along with the internal volumetric layout. Using this geometry-based approach, parameters such as wetted areas and cord lengths can be easily extracted for rapid external performance analyses, such as a parasite drag buildup. At the completion of the conceptual design phase, VSP can export its geometry to higher fidelity tools. This geometry tool was developed by NASA and is freely available to U.S. companies and universities. It has become integral to conceptual design in the Aeronautics Systems Analysis Branch (ASAB) here at NASA Langley Research Center and is currently being used at over 100 universities, aerospace companies, and other government agencies. This paper focuses on the use of VSP in recent NASA conceptual design studies to facilitate geometry-centered design methodology. Such a process is shown to promote greater levels of creativity, more rapid assessment of critical design issues, and improved ability to quickly interact with higher order analyses. A number of VSP vehicle model examples are compared to CAD-based conceptual design, from a designer perspective; comparisons are also made of the time and expertise required to build the geometry representations as well.
Document ID
20100003048
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Fredericks, William J.
(NASA Langley Research Center Hampton, VA, United States)
Antcliff, Kevin R.
(NASA Langley Research Center Hampton, VA, United States)
Costa, Guillermo
(NASA Langley Research Center Hampton, VA, United States)
Deshpande, Nachiket
(NASA Langley Research Center Hampton, VA, United States)
Moore, Mark D.
(NASA Langley Research Center Hampton, VA, United States)
Miguel, Edric A. San
(NASA Langley Research Center Hampton, VA, United States)
Snyder, Alison N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 4, 2010
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2010-658
LF99-9983
Meeting Information
Meeting: 48th AIAA Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.07.13.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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