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Ablator Modeling: Why Not Much Has Changed Over the Past 45 plus YearsIn the late 1950s, the earliest models describing the thermal response of ablative materials were based on the heat of ablation concept, which is an empirical approach that was reasonable for the types of materials of interest at that time. In the early-mid 60s the models were expanded to include pyrolysis since organic resin composites became the TPS materials of interest. However, surface recession was still predominantly modeled via empirical correlation. The development of the 1-D CMA finite difference code in the mid-late 60s introduced the thermochemical ablation approach for gas/surface interactions. Since that time investigators have developed finite volume and finite element codes, in 1-D, 2-D and 3-D, but the basic modeling has not evolved significantly. Models describing internal gas pressure due to pyrolysis, particle impact erosion, in-depth radiant transport, etc., have been added to address specific problems, but the fundamental modeling has not evolved. The reasons for this stagnation, as viewed by the author, will be described.
Document ID
20110012046
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Laub, B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2011
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN3105
Report Number: ARC-E-DAA-TN3105
Meeting Information
Meeting: 4th AF/SNL/NASA Ablation Workshop
Location: Albuquerque, NM
Country: United States
Start Date: March 1, 2011
End Date: March 3, 2011
Sponsors: Department of the Air Force, NASA Headquarters
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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