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Development and Verification of the Charring Ablating Thermal Protection Implicit System SolverThe development and verification of the Charring Ablating Thermal Protection Implicit System Solver is presented. This work concentrates on the derivation and verification of the stationary grid terms in the equations that govern three-dimensional heat and mass transfer for charring thermal protection systems including pyrolysis gas flow through the porous char layer. The governing equations are discretized according to the Galerkin finite element method with first and second order implicit time integrators. The governing equations are fully coupled and are solved in parallel via Newton's method, while the fully implicit linear system is solved with the Generalized Minimal Residual method. Verification results from exact solutions and the Method of Manufactured Solutions are presented to show spatial and temporal orders of accuracy as well as nonlinear convergence rates.
Document ID
20110000471
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Amar, Adam J.
(NASA Johnson Space Center Houston, TX, United States)
Calvert, Nathan D.
(NASA Johnson Space Center Houston, TX, United States)
Kirk, Benjamin S.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
JSC-CN-22416
Report Number: JSC-CN-22416
Meeting Information
Meeting: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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