Nodal Integral Method Using Quadrilateral Elements for Transport Equations: Part 2-Navier-Stokes Equations

2013 ◽  
Vol 64 (1) ◽  
pp. 22-47 ◽  
Author(s):  
Neeraj Kumar ◽  
Suneet Singh ◽  
J. B. Doshi
AIAA Journal ◽  
1982 ◽  
Vol 20 (3) ◽  
pp. 356-362 ◽  
Author(s):  
M. M. EIRefaee ◽  
J. C. Wu ◽  
S. G. Lekoudis

1994 ◽  
Vol 116 (4) ◽  
pp. 870-876 ◽  
Author(s):  
Ko-Foa Tchon ◽  
Ion Paraschivoiu

In order to study the dynamic stall phenomenon on a Darrieus wind turbine, the incompressible flow field around a moving airfoil is simulated using a noninertial stream function-vorticity formulation of the two-dimensional unsteady Navier-Stokes equations. Spatial discretization is achieved by the streamline upwind Petrov-Galerkin finite element method on a hybrid mesh composed of a structured region of quadrilateral elements in the vicinity of solid boundaries, an unstructured region of triangular elements elsewhere, and a layer of infinite elements surrounding the domain and projecting the external boundary to infinity. Temporal discretization is achieved by an implicit second order finite difference scheme. At each time step, a nonlinear algebraic system is solved by a Newton method. To accelerate computations, the generalized minimum residual method with an incomplete triangular factorization preconditioning is used to solve the linearized Newton systems. The solver is applied to simulate the flow around a NACA 0015 airfoil in Darrieus motion and the results are compared to experimental observations. To the authors’ knowledge, it is the first time that the simulation of such a motion has been performed using the Navier-Stokes equations.


Author(s):  
Charles G. Speziale

The high-Reynolds-number turbulent flows of technological importance contain such a wide range of excited length and time scales that the application of direct or large-eddy simulations is all but impossible for the foreseeable future. Reynolds stress models remain the only viable means for the solution of these complex turbulent flows. It is widely believed that Reynolds stress models are completely ad hoc, having no formal connection with solutions of the full Navier-Stokes equations for turbulent flows. While this belief is largely warranted for the older eddy viscosity models of turbulence, it constitutes a far too pessimistic assessment of the current generation of Reynolds stress closures. It will be shown how secondorder closure models and two-equation models with an anisotropic eddy viscosity can be systematically derived from the Navier-Stokes equations when one overriding assumption is made: the turbulence is locally homogeneous and in equilibrium. A brief review of zero equation models and one equation models based on the Boussinesq eddy viscosity hypothesis will first be provided in order to gain a perspective on the earlier approaches to Reynolds stress modeling. It will, however, be argued that since turbulent flows contain length and time scales that change dramatically from one flow configuration to the next, two-equation models constitute the minimum level of closure that is physically acceptable. Typically, modeled transport equations are solved for the turbulent kinetic energy and dissipation rate from which the turbulent length and time scales are built up; this obviates the need to specify these scales in an ad hoc fashion. While two-equation models represent the minimum acceptable closure, second-order closure models constitute the most complex level of closure that is currently feasible from a computational standpoint. It will be shown how the former models follow from the latter in the equilibrium limit of homogeneous turbulence. However, the two-equation models that are formally consistent with second-order closures have an anisotropic eddy viscosity with strain-dependent coefficients - a feature that most of the commonly used models do not possess.


Author(s):  
B. Noll ◽  
H. Schütz ◽  
M. Aigner

In the paper it is shown that statistical averaging of transport equations (URANS = Unsteady Reynolds Averaged Navier Stokes) imposes no inherent restriction concerning the ability to predict periodic or other deterministic transient flow processes. This even holds for periodic oscillations at relatively high frequencies lying in the spectral range of the inertial sub-range of flow turbulence. As an application, the unsteady behaviour of an isothermal swirling air flow through and behind an airblast-atomizer of a design typical for modern aeroengine combustors is treated. This flow exhibits self-excited oscillations at a frequency of 2.8 kHz. Computations of this flow behaviour based on the numerical solution of the unsteady statistically averaged Navier-Stokes equations are presented. The turbulence model employed in the computations is a k,ε-model modification for swirling flows. The transport equations are discretized by a Finite-Volume method on a curvilinear grid. Calculated mean velocity profiles as well as the predicted dynamic flow behaviour at the nozzle exit agree very well with appropriate LDV- and microphone-measurements.


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