Analysis of the linearly extrapolated BDF2 fully discrete Modular Grad-div stabilization method for the micropolar Navier-Stokes equations

We investigate a fully discrete modular grad-div (MGD) stabilization algorithm for solving the incompressible micropolar Navier-Stokes equations (IMNSE) model, which couples the incompressible Navier-Stokes equations and the angular momentum equation together. The mixed finite element (FE) method is applied for the spatial discretization. The time discretization is based on the BDF2 implicit scheme for the linear terms and the two-step linearly extrapolated scheme for the convective terms. The considered algorithm constitutes two steps, which involve a post-processing step for linear velocity. First, we decouple the fully coupled IMNSE model into two smaller sub-physics problems at each time step (one is for the linear velocity and pressure, the other is for the angular velocity), which reduces the size of the linear systems to be solved and allows for parallel computing of the two sub-physics problems. Then, in the post-processing step, we only need to solve a symmetrical positive determined grad-div system of linear velocity at each time step, which does not increase the computational complexity by much. However, the post-processing step can improve the solution quality of linear velocity. Moreover, we obtain unconditional stability, and error estimates of the linear velocity and angular velocity. Finally, several numerical experiments involving three-dimensional and two-dimensional settings are used to validate the theoretical findings and demonstrate the benefits of the modular grad-div (MGD) stabilization algorithm

On Numerical Algorithms for Fluid Flow Regularization Models

This thesis studies regularization models as a way to approximate a flow simulation at a lower computational cost. The Leray model is more easily computed than the Navier-Stokes equations (NSE), and it is more computationally attractive than the NS-α regularization because it admits a natural linearization which decouples the mass/momentum system and the filter system, allowing for efficient and stable computations. A major disadvantage of the Leray model lies in its inaccuracy. Thus, we study herein several methods to improve the accuracy of the model, while still retaining many of its attractive properties. This thesis is arranged as follows. Chapter 2 gives notation and preliminary results to be used in subsequent chapters. Chapter 3 investigates a nonlinear filtering scheme using the Vreman and Q-criteria based indicator functions. We define these indicator functions, prove stability and state convergence of the scheme to the NSE, and provide several numerical experiments which demonstrate its effectiveness over NSE and Leray calculations on coarse meshes. Chapter 4 investigates a deconvolution-based indicator function. We prove stability and convergence of the resulting scheme, verify the predicted convergence rates, and provide numerical experiments which demonstrate this scheme\u27s effectiveness. Chapter 5 then extends this scheme to the magnetohydrodynamic equations. We prove stability and convergence of our algorithm, and verify the predicted convergence rates. Chapter 6 provides a study of the Leray-α model. We prove stability and convergence for the fully nonlinear scheme, prove conditional stability for a linearized and decoupled scheme, and provide a numerical experiment which compares our scheme with the usual Leray-α model. Specifically, we show that choosing β \u3c α does indeed improve accuracy in computations. Chapter 7 investigates the Leray model with fine mesh filtering. We prove stability and convergence of the algorithm, then verify the increased convergence rate associated with the finer mesh, as predicted by the analysis. Finally, we present a benchmark problem which demonstrates the effectiveness of filtering on a finer mesh

Commonwealth of Independent States aerospace science and technology, 1992: A bibliography with indexes

This bibliography contains 1237 annotated references to reports and journal articles of Commonwealth of Independent States (CIS) intellectual origin entered into the NASA Scientific and Technical Information System during 1992. Representative subject areas include the following: aeronautics, astronautics, chemistry and materials, engineering, geosciences, life sciences, mathematical and computer sciences, physics, social sciences, and space sciences

Aeronautical engineering: A continuing bibliography with indexes (supplement 322)

This bibliography lists 719 reports, articles, and other documents introduced into the NASA scientific and technical information system in Oct. 1995. Subject coverage includes: design, construction and testing of aircraft and aircraft engines; aircraft components, equipment, and systems; ground support systems; and theoretical and applied aspects of aerodynamics and general fluid dynamics