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Overview of the CHarring Ablator Response (CHAR) CodeAn overview of the capabilities of the CHarring Ablator Response (CHAR) code is presented. CHAR is a one-, two-, and three-dimensional unstructured continuous Galerkin finite-element heat conduction and ablation solver with both direct and inverse modes. Additionally, CHAR includes a coupled linear thermoelastic solver for determination of internal stresses induced from the temperature field and surface loading. Background on the development process, governing equations, material models, discretization techniques, and numerical methods is provided. Special focus is put on the available boundary conditions including thermochemical ablation, surface-to-surface radiation exchange, and flowfield coupling. Finally, a discussion of ongoing development efforts is presented.
Document ID
20150021133
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Amar, Adam J.
(NASA Johnson Space Center Houston, TX, United States)
Oliver, A. Brandon
(NASA Johnson Space Center Houston, TX, United States)
Kirk, Benjamin S.
(NASA Johnson Space Center Houston, TX, United States)
Salazar, Giovanni
(NASA Johnson Space Center Houston, TX, United States)
Droba, Justin
(HX5 Fort Walton Beach, FL, United States)
Date Acquired
November 12, 2015
Publication Date
June 13, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Numerical Analysis
Computer Programming And Software
Report/Patent Number
JSC-CN-34679
Meeting Information
Meeting: AIAA Thermophysics Conference
Location: Washington, D. C.
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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