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Titlebook: Analysis and Numerics for Conservation Laws; Gerald Warnecke Book 2005 Springer-Verlag Berlin Heidelberg 2005 astrophysics.calculus.comput

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樓主: solidity
21#
發(fā)表于 2025-3-25 05:46:44 | 只看該作者
22#
發(fā)表于 2025-3-25 10:58:01 | 只看該作者
High-resolution Simulation of Detonations with Detailed Chemistry,re solution strategy for the Euler equations of thermally perfect gas-mixtures with detailed chemical kinetics that is based on a highly adaptive finite volume method for blockstructured Cartesian meshes. Large-scale simulations of unstable detonation structures of hydrogen-oxygen detonations demonstrate the efficiency of the approach in practice.
23#
發(fā)表于 2025-3-25 13:13:42 | 只看該作者
24#
發(fā)表于 2025-3-25 17:31:46 | 只看該作者
Meshless Methods for Conservation Laws,uds. Details of the derivation and numerical examples are presented for the case of incompressible, viscous, two-phase flow. In the case of FVPM, our main focus lies on the derivation of stability estimates.
25#
發(fā)表于 2025-3-25 22:55:00 | 只看該作者
26#
發(fā)表于 2025-3-26 00:53:32 | 只看該作者
Bernhard E. Keiser,Eugene Strangeales is determined by the interaction of turbulent fluctuations. Resulting lane-like and curled dust distributions combine to larger and larger structures. We compile necessary criteria for a subgrid model in the frame of large scale simulations as result of our study on small scale turbulence in dust forming gases.
27#
發(fā)表于 2025-3-26 06:18:49 | 只看該作者
28#
發(fā)表于 2025-3-26 11:35:14 | 只看該作者
The Multi-Scale Dust Formation in Substellar Atmospheres,ales is determined by the interaction of turbulent fluctuations. Resulting lane-like and curled dust distributions combine to larger and larger structures. We compile necessary criteria for a subgrid model in the frame of large scale simulations as result of our study on small scale turbulence in dust forming gases.
29#
發(fā)表于 2025-3-26 16:17:53 | 只看該作者
Numerics for Magnetoplasmadynamic Propulsion,erational envelope and the thruster lifetime — is the depletion of density and charge carriers in front of the anode because of the pinch effect..The calculated thrust data agree well with experimental values, so that the newly developed method can be used for the design and optimization of new thrusters.
30#
發(fā)表于 2025-3-26 17:14:51 | 只看該作者
Kinetic Schemes for Selected Initial and Boundary Value Problems,ntegrals of the kinetic phase density. (ii) Decomposition of the evolution into periods of free flight, which are interrupted by update times. (iii) At the update times the data are refreshed by the Maximum Entropy Principle.
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