FOLD SHAPE ANALYSIS: INSIGHTS FROM NUMERICAL MODELING OF FLEXURAL SLIP MULTILAYER BUCKLE FOLDS
For effective single layer buckle folds, which amplify the dominant wavelength, slip initiates early, chevron folds do not develop, and a transition from sinusoidal or parabolic to box folds is common. For lower amounts of slip, rounded box folds develop; increasing amounts of slip result in flat-topped box folds including M-shaped subsidiary folds. For true multilayer setups, both box folds and chevron folds develop for a variety of model setups. Box folds gradually develop through a progression from sinusoidal to parabolic to box folds. Key control parameters for the development of box folds are the ratio of incompetent layer thickness to competent layer thickness, s/h, the viscosity contrast, the friction coefficient, and the number of layers.
Systematic chevron folds featuring hinge collapse develop regardless of the initial perturbation used. The ratio s/h is a crucial parameter: for s/h>1, flexural flow dominates and slip is not initiated; for s/h<1, flexural slip initiates, and the lower s/h becomes, the more slip surfaces are activated. The results also document that flexural slip initiates during the later stages of folding and that sinusoidal or parabolic folds instantaneously change shape to chevron folds during a short period of slip initiation and termination, thus confirming the phenomenon of limb lock up.
The fold shapes from the numerical models are in good agreement with observations from the field and laboratory experiments and thus enable a quantitative assessment of dynamic fold development.