Stemming from a one-dimensional approach and thanks to a compact notation for the a priori kinematic field approximation over the beam cross-section, the model derivation is made general regardless the approximation order.
The feature of the umbilical cross section in the model is a large-diameter central pipe.
With its fluorescence quantum yield of ∼0.7−0.9, the two-photon action cross section for the model adduct is ∼20 GM, reasonable enough to be used for bioimaging.
The top surface and the alumina barrier layer were also flat. Figure 1a shows a schematic cross section of the model used in this first stage, where d int is the inter-pore distance, d p the pore diameter, t w the pore wall thickness, L is the pore length and t b is the barrier layer thickness.
A schematic cross section of the model including key dimensions and instrumentation is shown in Figure 4(b).
The Radar Cross Section model [35] aims to model the impact of the diffused reflections produced when a radio wave impinges on a non-uniform surface like a building.
An interacting-serial type model is constructed with step changes of tube size along the model, while the total cross-section of the model is kept constant.
For a given bridge deck cross-section the proposed model allows the numerical evaluation of the flutter derivatives, which is useful to characterize in an analytical way the stability conditions of the overall wind-induced bridge response.
To verify the effectiveness of SRM PFC3D models, the cross section of the PFC3D model was cut out for comparison with the CT image.
Fig. 3 Comparison of central cross sections for the models SH18CE (Takeuchi, 2007), SAW24B16 (Mégnin and Romanowicz, 2000), SB4L18 (Masters et al., 2000), S20RTS (Ritsema et al., 1999), and S362D1 (Gu et al., 2001).
Fig. 4 Comparison of integrated cross sections for the models SH18CE (Takeuchi, 2007), SAW24B16 (Mégnin and Romanowicz, 2000), SB4L18 (Masters et al., 2000), S20RTS (Ritsema et al., 1999), and S362D1 (Gu et al., 2001).
