2 edition of Time accurate simulation of compressible shear flows found in the catalog.
Time accurate simulation of compressible shear flows
by Turbulent Research Laboratory, School of Engineering and Applied Sciences, National Aeronautics and Space Administration, National Technical Information Service, distributor in Buffalo, N.Y, [Washington, DC, Springfield, Va
Written in English
|Statement||P. Givi ... [et al.].|
|Series||[NASA contractor report] -- NASA CR-193410., NASA contractor report -- NASA CR-193410.|
|Contributions||Givi, P., United States. National Aeronautics and Space Administration.|
|The Physical Object|
High-Speed Nozzle Flow. The design of nozzles for space rocket nozzles is an example of an application where compressible flow simulation are of high value. Testcampaigns for rocket nozzles are extremely complicated and expensive, which means that input from simulations are needed to be able to make desisions in eraly design phases. A simple second order accurate and fully Eulerian numerical method is presented for the simulation of multifluid compressible flows, governed by the stiffened gas equation of state, in hydrodynamic regime. Our numerical method relies on a second order Godunov-type scheme, with approximate Riemann solver for the resolution of conservation equations, and a set of nonconservative equations.
Large Eddy Simulation (LES) of compressible flows is still a widely unexplored area of research. The authors, whose books are considered the most relevant monographs in this field, provide the reader with a comprehensive state-of-the-art presentation of the available LES theory and application. Simulation of Sand Particles Flow Using a Weakly Compressible Smoothed Particle Hydrodynamics Method (WCSPH) is regarded for simulation and analysis. Accurate specification of different effective parameters on the properties of two-phase flows has considerable importance. Geometry effects on the interaction of two equal-sized drops in.
CiteSeerX - Document Details (Isaac Councill, Lee Giles, Pradeep Teregowda): In this paper, we perform a direct numerical simulation study to investigative the effect of compressibility on the flow over a backward-facing step. A spectral multidomain method is used for simulating the compressible flow at Reynolds number of over an open backward-facing step. Space-time correlation is a staple method for investigating the dynamic coupling of spatial and temporal scales of motion in turbulent flows. In this article, we review the space-time correlation models in both the Eulerian and Lagrangian frames of reference, which include the random sweeping and local straining models for isotropic and homogeneous turbulence, Taylor's frozen-flow model and.
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Get this from a library. Time accurate simulation of compressible shear flows. [P Givi; United States. National Aeronautics and Space Administration.;]. Time accurate simulations of compressible shear flows.
By Peyman Givi, Cyrus K. Madnia, Thomas J. Vidoni and Craig J. Steinberger. Abstract. The objectives of this research are to employ direct numerical simulation (DNS) to study the phenomenon of mixing (or lack thereof) in compressible free shear flows and to suggest new means of enhancing.
The simulation approaches have provided important insights into the dynamics of compressible homogeneous flows and now, inhomogeneous flows, and the averaged approaches have traditionally been the methodology used in replicating and predicting the more complex engineering flows.
The present simulations of the homogeneous shear problem augment and extend our previous results (, ) for compressible isotropic turbulence. The compressible Navier-Stokes equations are written in a frame of reference moving with the mean flow u.
We use a Fourier collocation method for the spatial discretization of the governing by: DIRECT SIMULATION OF COMPRESSIBLE TURBULENCE IN A SHEAR FLOW a S.
Sarkar, G. Erlebacher, and M.Y. Hussaini Institute for Computer Applications in Science and Engineering NASA Langley Research Center Hampton, VA ABSTRACT The purpose of this study is to investigate compressibility effects on the turbulence in homo-geneous shear flow. Hall, Edward Joseph, "Simulation of time-dependent compressible viscous flows using central and upwind-biased finite-difference techniques " ().Retrospective Theses and Dissertations.
Direct numerical simulation of a spatially developing compressible plane mixing layer: flow structures and mean flow properties 28 September | Journal of Fluid Mechanics, Vol. Improving the Simulation of the Acoustic Performance of Complex Silencers for.
CONTENTS vii In What Situations No Oblique Shock Exist or When. Upstream Mach Number, and Shock Angle, For Given Two Angles. The ﬁrst book devoted to CFD was written by Patrick Roache during a year-long visit to the Mechanical Engineering Department of the University of Kentucky during –71, and was published the following year .
Computing power at that time was still grossly inadequate for what we today would consider. Flow Simulation Technical Reference 1 • Steady-state and time-dependent fluid flows • Compressible gas and incompressible fluid flows • Subsonic, transonic, and supersonic gas flows • Free, forced, and mixed convection shear stress tensor, is.
The observation of Sarkar was confirmed by the study of Simone et al. (,“The Effect of Compressibility on Turbulent Shear Flow: A Rapid Distortion Theory and Direct Numerical Simulation Study,” J.
Fluid Mech.,p. ;“Etude Théorique et Simulation Numérique de la Turbulence Compressible en Présence de Cisaillement où de. The implication is that the turbulent simulation MUST be always three-dimensional, time accurate with extremely fine grids. MEB/3/GI 6 Direct Numerical Simulation The objective is to solve the time-dependent NS equations resolving ALL the scale (eddies) for a sufficient time interval so that the fluid Homogeneous shear flow 3.
The. Large-eddy simulations of the flow over a deep cavity are performed. The computations reproduce identically all the parameters of the experiment by Forestier and co-workers [J. Fluid Mech. (to be published)], including the high Reynolds number Re L =×10 5.
Spectra show an accurate prediction of the peak levels of the fundamental frequency and its first harmonics. Our two-dimensional numerical experiments are solved to a final dimensionless time of t=5. We clarify that the ℝ 2 simulation domain for all experiments is set in (x, y) ∈ [, ] × [, ] with N 2 =16 2 degrees of freedom.
Figure 1 represents a schematic expressing the initial conditions of our two-dimensional simulation. Time-accurate fluid-structure coupling for turbulent flows Hybrid-cartesian grid procedure for the simulation of compressible turbulent flows.
Philippe Geuzaine, Jean-André Essers. Pages Algorithm for construction of quasi-isometric grids in curvilinear quadrangular regions High reynolds number large-eddy simulation of free. This book is a sequel to "Large Eddy Simulation for Incompressible Flows", as most of the research on LES for compressible flows is based on variable density extensions of models, methods and.
This paper reports results from the numerical implementation and testing of the compressible large‐eddy simulation (LES) model described by Speziale et al. [Phys. Flu ()] and Erlebacher et al.
(to appear in J. Fluid Mech.). Relevant quantities from 32 3 ‘‘coarse grid’’ LES solutions are compared with results generated from 96 3 direct numerical simulations (DNS) of. This thesis describes the development of a numerical solution procedure which is valid for both incompressible flow and compressible flow at any Mach number.
Most of the available numerical methods are for incompressible flow or compressible flow only and density is usually chosen as a main dependent variable by almost all the methods developed for compressible flow.
Flow Control of Compressible Turbulent Shear Layers Transactions of the Japan Society of Mechanical Engineers Series B, Vol. 63, No. An experimental investigation of thermal mixing and combustion in supersonic flows.
() Compressible two-phase flow using a fourth order time-accurate TVD-SLIC method., () Physical modeling and numerical studies of three-dimensional non-equilibrium multi-temperature flows. The compressibility effects on the transition to turbulence in a spatially developing, compressible plane free shear layer are investigated via direct numerical simulation using a high-order.Numerical investigation of the compressible flow past an 18% thick circular-arc aerofoil was carried out using detached-eddy simulation for a free-stream Mach number M ∞ = and a Reynolds number Re = × 10 s have been validated carefully against experimental data.This book deals with an introduction to the flow of compressible substances (gases).
The main difference between compressible flow and almost incompressible flow is not the fact that compressibility has to be considered. Rather, the difference is in two phenomena that do not exist in incompressible flow. The first phenomenon is the very sharp discontinuity (jump) in the flow in .