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Titlebook: Dynamics of Compressible Fluids; A Textbook Oleksandr Girin Textbook 2022 The Editor(s) (if applicable) and The Author(s), under exclusive

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樓主: memoir
31#
發(fā)表于 2025-3-26 21:07:30 | 只看該作者
Governing Equations and?Initial-Boundary-Value Problems of special type are also formulated. The characteristics as potential branch-lines of solution and as a trajectory of possible weak discontinuities are discussed; relations along weak discontinuity are obtained. Problem of disintegration of arbitrary weak discontinuity is set and non-evolutionary c
32#
發(fā)表于 2025-3-27 03:11:31 | 只看該作者
33#
發(fā)表于 2025-3-27 08:38:45 | 只看該作者
Shock—Wave Flowslems of wave interactions yielding the wave effects are also considered: shock tube performance, the tube design, direct and inverse problems; shock wave reflection from rigid wall with amplification of its percussive action; shock wave interaction with contact surface; interaction of two shocks; sh
34#
發(fā)表于 2025-3-27 12:46:42 | 只看該作者
35#
發(fā)表于 2025-3-27 13:57:33 | 只看該作者
36#
發(fā)表于 2025-3-27 20:36:12 | 只看該作者
Cerebral Blood Flow Mapping the Brain,voir. Instead, to increase the flow velocity, one needs to apply a special nozzle. Subsonic (Venturi tube) and supersonic (Laval nozzle) outflow modes are considered. Nozzle calculation schemes are described; on-design and off-design nozzles are defined.
37#
發(fā)表于 2025-3-27 22:40:27 | 只看該作者
38#
發(fā)表于 2025-3-28 03:41:32 | 只看該作者
Lecture Notes in Computer Scienceimilar solution, which gives complete analysis of all solution cases where the final equilibrium state is found. System of equations for the sought waves and logic of the root finding are added. Description of a simpler acoustic approximation is given.
39#
發(fā)表于 2025-3-28 08:03:10 | 只看該作者
40#
發(fā)表于 2025-3-28 12:00:41 | 只看該作者
Jing He,Zhen Zhang,Yuanhui Xiao,Mian Wangction is found; steady expansion into vacuum is described as a limiting case. Plane supersonic outflow from a slit is described with “barrel”-flow formation bounded by free-surface. Main concepts of thin airfoil theory and problem formulation are listed. Thin profile streamlining in subsonic and sup
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