29th International Symposium on Shock Waves 2: Volume 2 - download pdf or read online
By Riccardo Bonazza, Devesh Ranjan
This court cases current the result of the twenty ninth foreign Symposium on surprise Waves (ISSW29) which used to be held in Madison, Wisconsin, u.s., from July 14 to July 19, 2013. It was once prepared through the Wisconsin surprise Tube Laboratory, that is a part of the school of Engineering of the college of Wisconsin-Madison. The ISSW29 interested by the next components: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, amenities, stream Visualization, Hypersonic stream, Ignition, effect and Compaction, business purposes, Magnetohydrodynamics, clinical and organic functions, Nozzle stream, Numerical tools, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer interplay, surprise Propagation and mirrored image, surprise Vortex interplay, surprise Waves in Condensed topic, surprise Waves in Multiphase circulate, in addition to surprise Waves in Rarefield stream. the 2 Volumes comprise the papers offered on the symposium and function a reference for the contributors of the ISSW 29 and contributors drawn to those fields.
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Additional resources for 29th International Symposium on Shock Waves 2: Volume 2
For example, the unsteady method badly smears the contact discontinuity between the slow compound wave and the right slow shock, but the self-similar method clearly distinguishes between the different waves. Additionally, the self-similar method provides improved resolution on more minor features. 5 0 0 −2 −1 0 ξ 1 2 −2 −1 ξ Fig. 2. Solid lines: self-similar solution. Dashed lines: unsteady solutions. Results of the test case by . 5 −2 −1 0 ξ 1 2 3 1 −3 −2 −1 ξ Fig. 3. Solid lines: self-similar solution.
Characterisation of the Cylindrical Riemann Problem in Magnetohydrodynamics 825 • Case 2: An azimuthal magnetic field B = B(r)ˆeθ is applied such that outside the interface |B| ∝ 1/r, while inside the interface |B| = 0. This is approximately equivalent to the field generated by a current running along the interface in a direction perpendicular to the plane. • Case 3: A saddle-shaped (hyperbolic) magnetic field, generated by an arrangement of four magnetic dipoles outside the physical domain. 3 Methodology The simulations discussed were conducted using a finite volume code  for solving the ideal compressible MHD equations using an unsplit upwinding method.
Vorticity is used in the left frame to clearly show the wave positions, including density laplacian magnitude to identify the contact surface. The flow immediately downstream of the shock is horizontally converging; to align the converging fluid streams, two additional reflected waves form. These waves move out- and downward, compressing the flow, and are thus slow shocks. These waves connect with the slow expansion wave structure away from θ = π /2, forming what appear to be singularities in curvature at the connection points.
29th International Symposium on Shock Waves 2: Volume 2 by Riccardo Bonazza, Devesh Ranjan