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CFD Script for Rapid TPS Damage AssessmentThis grid generation script creates unstructured CFD grids for rapid thermal protection system (TPS) damage aeroheating assessments. The existing manual solution is cumbersome, open to errors, and slow. The invention takes a large-scale geometry grid and its large-scale CFD solution, and creates a unstructured patch grid that models the TPS damage. The flow field boundary condition for the patch grid is then interpolated from the large-scale CFD solution. It speeds up the generation of CFD grids and solutions in the modeling of TPS damages and their aeroheating assessment. This process was successfully utilized during STS-134.
Document ID
20130014112
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
McCloud, Peter
(Boeing Co. Houston, TX, United States)
Date Acquired
August 27, 2013
Publication Date
July 1, 2013
Publication Information
Publication: NASA Tech Briefs, July 2013
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-24865-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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