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Molecular-Level Simulations of Turbulent Couette Flow Over A Thermal-Protection-System MaterialWe report flow statistics and visualizations from molecular-gas-dynamics simulations using the direct simulation Monte Carlo (DSMC) method for turbulent Couette flow in which the lower wall is replaced by a rough and permeable substrate obtained from a three-dimensional image scan of the low-density carbon reinforcement material FiberForm, used to manufacture NASA’s PICA thermal protection material. We focus on near-continuum conditions corresponding to modest global Reynolds numbers Re = 2800–9300 and supersonic Mach numbers Ma = 1.5–5. Additionally, we present permeability calculations for differing levels of rarefaction and assess the potential for noncontinuum effects on the overlying turbulent flow.
Document ID
20250009578
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Ryan M McMullen
(Sandia National Laboratories Albuquerque, United States)
Arnaud Borner
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Michail A Gallis
(Sandia National Laboratories Albuquerque, United States)
Date Acquired
September 25, 2025
Subject Category
Composite Materials
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: DSMC Conference
Location: Santa Fe, NM
Country: US
Start Date: September 28, 2025
End Date: October 1, 2025
Sponsors: Sandia National Laboratories
Funding Number(s)
CONTRACT_GRANT: DE-NA0003525
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
SPARTA
FiberForm
Turbulence
Couette flow
DSMC
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