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Numerical Modeling of Ablation Heat TransferA unique numerical method has been developed for solving one-dimensional ablation heat transfer problems. This paper provides a comprehensive description of the method, along with detailed derivations of the governing equations. This methodology supports solutions for traditional ablation modeling including such effects as heat transfer, material decomposition, pyrolysis gas permeation and heat exchange, and thermochemical surface erosion. The numerical scheme utilizes a control-volume approach with a variable grid to account for surface movement. This method directly supports implementation of nontraditional models such as material swelling and mechanical erosion, extending capabilities for modeling complex ablation phenomena. Verifications of the numerical implementation are provided using analytical solutions, code comparisons, and the method of manufactured solutions. These verifications are used to demonstrate solution accuracy and proper error convergence rates. A simple demonstration of a mechanical erosion (spallation) model is also provided to illustrate the unique capabilities of the method.
Document ID
20140008557
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ewing, Mark E.
(ATK Aerospace Systems Brigham City, UT, United States)
Laker, Travis S.
(ATK Aerospace Systems Brigham City, UT, United States)
Walker, David T.
(ATK Aerospace Systems Brigham City, UT, United States)
Date Acquired
June 30, 2014
Publication Date
May 1, 2013
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
M13-2514
Funding Number(s)
CONTRACT_GRANT: NAS8-97238
Distribution Limits
Public
Copyright
Public Use Permitted.
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