NASA NTRS · 19910042995
Regolith-structure modeling of lunar facilities
Abstract
The mechanical properties of lunar regolith are significantly different from terrestrial soils; at low stress levels, the ultimate strength envelope is highly nonlinear, and the material is essentially dilatant. The effects of platen friction, membrane confinement, and material self weight in triaxial tests have been shown to be of great significance in low stress level tests. An inverse identification technique has been devised to account for these effects where the load-displacement response of the entire specimen, including the boundary conditions and the self-weight, was analyzed by nonlinear finite element techniques so as to obtain true material parameters.
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Perkins, Steven W., Sture, Stein, Ko, Hon-Yim. 1990-01-01. Regolith-structure modeling of lunar facilities. https://ntrs.nasa.gov/citations/19910042995
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