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A Tutorial for Using the CGT Script Library to Generate and Assemble Overset MeshesThe purpose of this document is to introduce a new user to the procedures for overset CFD analysis by building scripts based on the CGT Script Library. Parameterized inputs are built into the steps of the process which include creation and manipulation of geometry, and surface and volume meshing. In preparation for performing computations in the flow solver, further steps are constructed for specification of inputs for domain connectivity, flow solver boundary conditions, and components for computation of aerodynamic forces/moments. The JCLV rocket will be used as an example geometry for this demonstration.
Document ID
20180004214
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Pandya, Shishir A.
(NASA Ames Research Center Moffett Field, CA, United States)
Chan, William M.
(NASA Ames Research Center Moffett Field, CA, United States)
Rogers, Stuart E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 6, 2018
Publication Date
April 1, 2018
Subject Category
Aeronautics (General)
Report/Patent Number
ARC-E-DAA-TN57092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Script
Tutorial
CGT
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