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Multi-Dimensional, Non-Pyrolyzing Ablation Test ProblemsNon-pyrolyzingcarbonaceous materials represent a class of candidate material for hypersonic vehicle components providing both structural and thermal protection system capabilities. Two problems relevant to this technology are presented. The first considers the one-dimensional ablation of a carbon material subject to convective heating. The second considers two-dimensional conduction in a rectangular block subject to radiative heating. Surface thermochemistry for both problems includes finite-rate surface kinetics at low temperatures, diffusion limited ablation at intermediate temperatures, and vaporization at high temperatures. The first problem requires the solution of both the steady-state thermal profile with respect to the ablating surface and the transient thermal history for a one-dimensional ablating planar slab with temperature-dependent material properties. The slab front face is convectively heated and also reradiates to a room temperature environment. The back face is adiabatic. The steady-state temperature profile and steady-state mass loss rate should be predicted. Time-dependent front and back face temperature, surface recession and recession rate along with the final temperature profile should be predicted for the time-dependent solution. The second problem requires the solution for the transient temperature history for an ablating, two-dimensional rectangular solid with anisotropic, temperature-dependent thermal properties. The front face is radiatively heated, convectively cooled, and also reradiates to a room temperature environment. The back face and sidewalls are adiabatic. The solution should include the following 9 items: final surface recession profile, time-dependent temperature history of both the front face and back face at both the centerline and sidewall, as well as the time-dependent surface recession and recession rate on the front face at both the centerline and sidewall. The results of the problems from all submitters will be collected, summarized, and presented at a later conference.
Document ID
20160012295
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Risch, Tim
(NASA Armstrong Flight Research Center Edwards, CA United States)
Kostyk, Chris
(NASA Armstrong Flight Research Center Edwards, CA United States)
Date Acquired
October 12, 2016
Publication Date
October 5, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
DFRC-E-DAA-TN36057
Report Number: DFRC-E-DAA-TN36057
Meeting Information
Meeting: Ablation Workshop
Location: Tucson, AZ
Country: United States
Start Date: October 5, 2016
End Date: October 6, 2016
Sponsors: Sandia National Labs., NASA Headquarters, Kentucky Univ., Raytheon Co., Arizona Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Ablation
Test Data
Hypersonics
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