Although numerous transfer zones of deformation have been observed in
thrust wedges, their mechanisms and conditions of development are Poor
ly understood. In this paper three basic questions are addressed: (1)
what are the parameters controlling the genesis of transfer zones? (2)
what are the kinematics of thrust propagation during transfer zone de
velopment? and (3) which kinds of geological structure link the two co
mpartments on either side of the transfer zone? We attempted to solve
these problems using a 3-D experimental approach. Sand models were use
d to simulate the foreland, a rigid, but mobile, backstop was used to
produced a thrust Coulomb wedge which was studied during the various s
tages of its formation. Shortening led to the development of transfer
zones in the wedge, separating two domains of homogenous behaviour and
connecting thrust planes in different domains. The experimental resul
ts show that the development of transfer zones is controlled by mechan
ical and/or geometrical parameters such as: (1) variations in the sedi
mentary thickness in the foreland; (2) the steepness of the backstop;
(3) domains with different basal friction in the foreland; (4) kinked
backstop geometry. During deformation of the models, two types of thru
st sequence were identified: alternative thrust propagations on both s
ides of the transfer zone and synchronous thrust propagations which ar
e anastomosed within the transfer zone. 3-D reconstructions revealed t
hat the thrust deformations observed in the transfer zone are oblique
ramps. The frontal thrust bending of the Barbados accretionary complex
, as well as the imbrication of thrust in the ''Castellane'' arc and t
he oblique ramp in the Zanskar Range, are discussed in relation to the
mechanisms and structures revealed by the models. The results of anal
ogue modelling suggest that the development of transfer zones is direc
tly linked to variations in the boundary conditions (mechanical and/or
geometrical) between two adjacent parts of a thrust wedge.