A Study of Ablation-Flowfield Coupling Relevant to the Orion HeatshieldThe coupled interaction between an ablating surface and the surrounding aerothermal environment is studied. An equilibrium ablation model is coupled to the LAURA flowfield solver, which allows the char ablation rate (m-dot(sub c)) to be computed as part of the flowfield solution. The wall temperature (T(sub w)) and pyrolysis ablation rate (m-dot(sub g)) may be specified by the user, obtained from the steady-state ablation approximation, or computed from a a material response code. A 32 species thermochemical nonequilibrium flowfield model is applied, which permits the treatment of C, H, O, N, and Si containing species. Coupled ablation cases relevant to the Orion heatshield are studied. These consist of diffusion-limited oxidation cases with Avcoat as the ablation material. The m-dot(sub c) values predicted from the developed coupled ablation analysis were compared with those obtained from a typical uncoupled ablation analysis. The coupled results were found to be as much as 50% greater than the uncoupled values. This is shown to be a result of the cumulative effect of the two fundamental approximations inherent in the uncoupled analysis.
Document ID
20090025449
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Johnston, Christopher O. (NASA Langley Research Center Hampton, VA, United States)
Gnoffo, Peter A. (NASA Langley Research Center Hampton, VA, United States)
Mazaheri, Alireza (Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 22, 2009
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
LF99-9071Report Number: LF99-9071
Meeting Information
Meeting: 41st AIAA Thermophysics Conference
Location: San Antonio, TX
Country: United States
Start Date: June 22, 2009
End Date: June 25, 2009
Sponsors: American Inst. of Aeronautics and Astronautics