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Various dissolution theories provide insight into the factors that influence the dissolution rate. Danckwerts' Model suggests that turbulence, rather than a stagnant layer, characterizes the dissolution medium at the solid-liquid interface. In this model, the agitated solvent contains macroscopic packets that move to the interface via eddy currents, facilitating the absorption and delivery of the drug to the bulk solution. The regular replenishment of solvent packets maintains the...
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Multicompartment Models: Overview01:14

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Related Experiment Video

Updated: Dec 18, 2025

Author Spotlight: Evaluation of Protein-Condensate Dynamics in Live Human Cells
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Consistent kinetic-continuum dissociation model. II. Continuum formulation and verification.

Narendra Singh1, Thomas Schwartzentruber1

  • 1Department of Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, Minnesota 55455, USA.

The Journal of Chemical Physics
|June 15, 2020
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Summary
This summary is machine-generated.

A new non-equilibrium chemical kinetics model, validated with molecular simulations, identifies key physics for hypersonic flows. This simplified model integrates into computational fluid dynamics for efficient analysis.

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Area of Science:

  • Chemical Kinetics
  • Computational Fluid Dynamics
  • Hypersonic Flow Physics

Background:

  • Non-equilibrium chemical kinetics models are crucial for accurately simulating high-enthalpy gas flows.
  • Existing models may not fully capture the complex physics involved in phenomena like hypersonic reentry.
  • Ab initio simulation data offers a foundation for developing more predictive kinetic models.

Purpose of the Study:

  • To implement and verify a recently developed non-equilibrium chemical kinetics model.
  • To identify dominant physical phenomena, including rotational energy effects and non-Boltzmann distributions.
  • To propose a simplified model for integration into large-scale computational fluid dynamics (CFD) simulations.

Main Methods:

  • Implementation of a non-equilibrium chemical kinetics model based on ab initio data.
  • Verification of the model's predictive capabilities using direct molecular simulation data.
  • Analysis of simulation results to identify key physical parameters and effects.

Main Results:

  • The model successfully captures essential physics, highlighting the necessity of a rotational energy equation.
  • Quantitative insights into the role of non-Boltzmann effects in hypersonic flows were obtained.
  • A simplified kinetic model was developed for efficient integration into existing CFD solvers.

Conclusions:

  • The implemented non-equilibrium chemical kinetics model provides accurate predictions for hypersonic flows.
  • The simplified model offers a computationally inexpensive way to incorporate detailed kinetics into CFD.
  • This approach enhances the analysis of hypersonic phenomena without significant additional computational cost.