TL;DR: In this paper, a comparison of numerical methods for simulating hydrodynamics with strong shocks in two dimensions is presented and discussed, and three approaches to treating discontinuities in the flow are discussed.
TL;DR: In this article, the Shallow Water Equations are expressed as linearised shallow water equations, and the Riemann solver is used to solve the problem of Dam-Break Modelling.
Abstract: Preface. Introduction. The Shallow Water Equations. Properties of the Equations. Linearised Shallow Water. Exact Riemann Solver: Wet Bed. Exact Riemann Solver: Dry Bed. Tests with Exact Solution. Basics on Numerical Methods. First-Order Methods. Approximate Riemann Solvers. TVD Methods. Sources and Multi-Dimensions. Dam-Break Modelling. Mach Reflection of Bores. Concluding Remarks. References. Index.
TL;DR: In this paper, recent developments in three dimensional and unsteady turbulence boundary layer computations are discussed, including the physics of convention solidification interaction, the continental shelf bottom boundary layer, gravity currents in rotating systems, eddies, waves, circulation, and mixing.
Abstract: This book covers the following topics: recent developments in three dimensional and unsteady turbulence boundary-layer computations; flows far from equilibrium via molecular dynamics; physics of convention-solidification interaction; the continental shelf bottom boundary layer; gravity currents in rotating systems; strange attractors in fluids: another view; eddies, waves, circulation, and mixing: statistical geofluid mechanics; regular and mach reflection of shock waves; ship propellers; coherent structures; the critical layer and stability; general circulation of the oceans; characteristic-based schemes for the euler equations; vortex flows in aerodynamics; steady and unsteady boundary-layer separation; and wind wave prediction.
TL;DR: In this article, the authors derived a scaling formula that the intensity of shock associated noise varies as (Mj2 − Md2)2 where Mj and Md are the fully expanded jet operating Mach number and nozzle design Mach number, respectively.
TL;DR: In this article, the sound generated by the interaction of two identical thin vortex rings was analyzed and it was shown that each vortex can be replaced acoustically by a dipole related to the impulse of the vortex.
Abstract: A transformation is described which relates the sound generated by low Mach number flow to the flow vorticity. For compact flow fields the apparent sound source is of quadrupole type and linear in the vorticity and therefore also linear in the flow velocity. This scheme is applied to the sound generated by the interaction of two identical thin vortex rings. Then a flow field with a number of compact vortices is discussed. It is found that each vortex can be replaced acoustically by a dipole related to the impulse of the vortex, plus the quadrupole just mentioned plus a spherically symmetric sound source related to the energy of the vortex. An application to low Mach number free-space turbulence shows that the generated sound is related to the vorticity correlation tensor.