2007
DOI: 10.1016/j.ces.2006.11.057
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Modeling and analysis of local hot spot formation in down-flow adiabatic packed-bed reactors

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Cited by 35 publications
(20 citation statements)
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“…The fluid interface is compressed and stretched at the flow stagnation points at a stretching and compression rates = q x ∕ x = − q z ∕ z. This forms hot spots, i.e., regions where mixing and reaction are maximum [Agrawal et al, 2007;Gérard et al, 2012], which follow the strain rate distribution (Figures 2a-2c). The hot spots appear on either side of the stagnation points (Figures 2d) where the compression of the boundary layer is highest.…”
Section: Mixing and Dissolution Patternsmentioning
confidence: 99%
“…The fluid interface is compressed and stretched at the flow stagnation points at a stretching and compression rates = q x ∕ x = − q z ∕ z. This forms hot spots, i.e., regions where mixing and reaction are maximum [Agrawal et al, 2007;Gérard et al, 2012], which follow the strain rate distribution (Figures 2a-2c). The hot spots appear on either side of the stagnation points (Figures 2d) where the compression of the boundary layer is highest.…”
Section: Mixing and Dissolution Patternsmentioning
confidence: 99%
“…Previous studies were focused on linear analysis of the first four modes (see Figure 1 with the corresponding μ mn ) in either 3D16, 27, 28 or shallow reactor models15, 16, 29, 30 and did not simulate patterns. Linear analysis suggests formation of moving nonrotating patterns of the form (2) while the unstable domains of certain modes were quite similar in 3D and SR models.…”
Section: Introductionmentioning
confidence: 99%
“…fully developed or simultaneously developing boundary layers) but are independent of channel geometry. For the case of shallow packed-beds, the form of the second term is different, where the exponents are different on the velocity (or Reynolds number) and diffusivity (or Schmidt/Prandtl number), see for example, Agrawal et al [28]. Again, this new form does not alter any of qualitative bifurcation features studied here].…”
Section: Model Developmentmentioning
confidence: 83%
“…Regarding the accuracy (and validity) of the present model with respect to simpler or more complex models, the following comments (which are substantiated in references [22][23][24][25][26][27][28][29][30][31][32]) are appropriate: (i) The simplest of the models, namely the one dimensional pseudo-homogeneous plug flow model is structurally unstable and does not show ignition/extinction but only parametric sensitivity (ii) The pseudo-homogeneous model with no axial gradients (which is included as a special case of our model when interphase gradients are negligible) is robust but is good only for very small axial length scales and hydraulic diameters (micro-channels) [Remark: Structural stability or robustness here implies that the bifurcation and/or qualitative features do not change when the model is perturbed by including spatial gradients or other phenomena as long as the perturbations are small, see [30]] (iii) The 2-D boundary layer models (of parabolic type) that ignore axial diffusion (conduction) are structurally unstable, index infinity differential-algebraic system (and are not initial value problems). Further, as explained in the literature articles [23,26], most computational codes do not consider the Gibbs' phenomenon (which does not disappear even for arbitrarily small mesh size and leads to incorrect fluxes and temperature overshoot at the point of ignition) and compute only a single solution.…”
Section: Model Developmentmentioning
confidence: 98%