High-Order and Efficient Methods for the Vorticity Formulation of the Euler Equations
نویسندگان
چکیده
In this work, the authors develop new methods for the accurate and efficient solution of the two-dimensional, incompressible Euler equations in the vorticity form. Here, the velocity is recovered directly from the Biot-Savart relation with vorticity, and the vorticity is evolved through its transport equation. Using a generalized Poisson summation formula, the full asymptotic error expansion is constructed for the second-order point vortex approximation to the Biot-Savart integral over a rectangular grid. The expansion is in powers of h2, and its coefficients depend linearly upon only local derivatives of the vorticity. In particular , the second-order term depends only upon the vorticity gradient. Except at second-order, the coefficients also involve rapidly convergent, two-dimensional lattice sums. At second-order, the sum is conditionally con-vergent, but can be calculated easily and rapidly. Therefore, we can remove the second-order term explicitly from the point vortex approximation to obtain a fourth-order discretization. In the special case of a square grid, the second-order error term is orthogonal to the vorticity gradient. The convective derivative ofvorticity is thus calculated to fourth order using the unmodified point vortex approximation and automatically yields a fourth-order evolution. These methods have been implemented. For the vorticity transport equation, the point vortex sums are evaluated very rapidly using the fast Fourier transform (FFT) algorithm, and vorticity gradients are approximated using high-order difference methods. With high resolution, the authors solve numerically the roll-up of a thin layer of vorticity through the Kelvin-Helmholtz instability, and the interaction of two oppositely signed vortices driven together under an external strain flow. In the latter case, a simple time dependence of the grid is introduced to maintain resolution of the flow.
منابع مشابه
A Hamiltonian Vorticity-dilatation Formulation of the Compressible Euler Equations
Using the Hodge decomposition on bounded domains the compressible Euler equations of gas dynamics are reformulated using a density weighted vorticity and dilatation as primary variables, together with the entropy and density. This formulation is an extension to compressible flows of the well-known vorticity-stream function formulation of the incompressible Euler equations. The Hamiltonian and a...
متن کاملA Fast Immersed Boundary Fourier Pseudo-spectral Method for Simulation of the Incompressible Flows
Abstract The present paper is devoted to implementation of the immersed boundary technique into the Fourier pseudo-spectral solution of the vorticity-velocity formulation of the two-dimensional incompressible Navier-Stokes equations. The immersed boundary conditions are implemented via direct modification of the convection and diffusion terms, and therefore, in contrast to some other similar ...
متن کاملComparison of three different numerical schemes for 2D steady incompressible lid-driven cavity flow
In this study, a numerical solution of 2D steady incompressible lid-driven cavity flow is presented. Three different numerical schemes were employed to make a comparison on the practicality of the methods. An alternating direction implicit scheme for the vorticity-stream function formulation, explicit and implicit schemes for the primitive variable formulation of governing Navier-Stokes equatio...
متن کاملThe Formation of Shock Waves in the Presence of Vorticity
In his 2007 monograph, D. Christodoulou proved a breakthrough result giving a complete description of the formation of shock waves, starting from small, regular initial conditions, in solutions to the relativistic Euler equations. In 2014, Christodoulou–Miao extended the result to the nonrelativistic compressible Euler equations. In both works, the assumptions on the initial conditions caused t...
متن کاملAerodynamic Design Optimization Using Genetic Algorithm (RESEARCH NOTE)
An efficient formulation for the robust shape optimization of aerodynamic objects is introduced in this paper. The formulation has three essential features. First, an Euler solver based on a second-order Godunov scheme is used for the flow calculations. Second, a genetic algorithm with binary number encoding is implemented for the optimization procedure. The third ingredient of the procedure is...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید
ثبت ناماگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید
ورودعنوان ژورنال:
- SIAM J. Scientific Computing
دوره 14 شماره
صفحات -
تاریخ انتشار 1993