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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 a modest global Reynolds number Re = 2800 and supersonic Mach number Ma = 1.5. Additionally, we present permeability calculations for differing levels of rarefaction and assess the potential for noncontinuum effects on the overlying turbulent flow.
Document ID
20240014754
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
November 19, 2024
Subject Category
Composite Materials
Fluid Mechanics and Thermodynamics
Report/Patent Number
R36.00001
Meeting Information
Meeting: 77th Annual Meeting of the APS Division of Fluid Dynamics
Location: Salt Lake City, UT
Country: US
Start Date: November 24, 2024
End Date: November 26, 2024
Sponsors: American Physical Society
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
CONTRACT_GRANT: DE-NA0003525
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
Couette flow
Turbulence
FiberForm
SPARTA
DSMC
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