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		<title>Aerospace - Revision history</title>
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		<updated>2026-05-27T16:41:27Z</updated>
		<subtitle>Revision history for this page on the wiki</subtitle>
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		<id>https://www.clustermonkey.net/cdp/index.php?title=Aerospace&amp;diff=2799&amp;oldid=prev</id>
		<title>Deadline: added su2 and openvsp</title>
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				<updated>2012-12-27T20:38:48Z</updated>
		
		<summary type="html">&lt;p&gt;added su2 and openvsp&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;* [http://su2.stanford.edu/ SU2] is the Stanford University Unstructured (SU2) suite is an open-source collection of software tools written in C++ for performing Partial Differential Equation (PDE) analysis and solving PDE-constrained optimization problems. The toolset is designed with computational fluid dynamics and aerodynamic shape optimization in mind, but it is extensible (and has been extended) to treat arbitrary sets of governing equations such as electrodynamics, chemically reacting flows, and many others.&lt;br /&gt;
&lt;br /&gt;
* [http://www.openvsp.org/ OpenVSP] is a parametric aircraft geometry tool. OpenVSP allows the user to create a 3D model of an aircraft defined by common engineering parameters. This model can be processed into formats suitable for engineering analysis. The predecessors to OpenVSP have been developed by J.R. Gloudemans and others for NASA since the early 1990's. On January 10 2012, OpenVSP was released as an open source project under the NASA Open Source Agreement (NOSA) version 1.3.&lt;/div&gt;</summary>
		<author><name>Deadline</name></author>	</entry>

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