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Differences caused by non-catalytic vs. fully catalytic wall boundary conditions were assessed using CFD for a 2D-wedge model for a range of Mach numbers (7 < Mach < 10) and altitudes (25 km < Alt. < 45 km). We found oxygen recombination coefficient must be accurate O(~1e-3) to produce a distinguishable solution in-between both extremes, non and fully catalytic, assumptions.

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This page is a summary of: Investigation of Partially Catalytic Boundary Conditions for High-Speed Flows, Journal of Thermophysics and Heat Transfer, January 2026, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.t7352.
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