gene-therapy
发表于 2025-3-26 21:07:30
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
Adulterate
发表于 2025-3-27 03:11:31
http://reply.papertrans.cn/29/2841/284046/284046_32.png
隐士
发表于 2025-3-27 08:38:45
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
monopoly
发表于 2025-3-27 12:46:42
http://reply.papertrans.cn/29/2841/284046/284046_34.png
BAIT
发表于 2025-3-27 13:57:33
http://reply.papertrans.cn/29/2841/284046/284046_35.png
Mets552
发表于 2025-3-27 20:36:12
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.
GLUE
发表于 2025-3-27 22:40:27
http://reply.papertrans.cn/29/2841/284046/284046_37.png
ULCER
发表于 2025-3-28 03:41:32
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.
不可侵犯
发表于 2025-3-28 08:03:10
http://reply.papertrans.cn/29/2841/284046/284046_39.png
魔鬼在游行
发表于 2025-3-28 12:00:41
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