Results 11 to 20 of about 1,105,756 (226)
On Alternative Setups of the Double Mach Reflection Problem [PDF]
Journal of Scientific Computing, 2018 zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Vevek US, Bin Zang, Tze How New
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Interaction between Shock Waves Travelling in the Same Direction
Fluids, 2021 In this paper, we study the intersection (interaction) between several steady shocks traveling in the same direction. The interaction between overtaking shocks may be regular or irregular. In the case of regular reflection, the intersection of overtaking
Pavel Bulat +2 more
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Transition Between Regular Reflection and Mach Reflection in the Dual-Solution Domain [PDF]
, 2007 A study of the shock-reflection domain for steady flow is presented. Conditions defining boundaries between different possible shock-reflection solutions are given, and where possible, simple analytic expressions for these conditions are presented. A new,
Mouton, Christopher Andre
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Investigation of the Slipstream in Mach Reflections
JSME international journal. Ser. 2, Fluids engineering, heat transfer, power, combustion, thermophysical properties, 1988 A slipstream emanating from a triple point in the Mach reflection of a shock wave, which is assumed to be a discontinuous surface in the three-shock theory, from a high-speed mixing layer. In the present paper, the slipstream in the Mach reflection has been investigated in detail and visualized by means of the shadowgraph method.
HIRAHARA, Hiroyuki +2 more
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Mach-Reflection as a Diffraction Problem
Coastal Engineering 1976, 1976 As under oblique wave approach water waves are reflected by a vertical wall, a wave branching effect (stem) develops normal to the reflecting wall. The waves progressing along the wall will steep up. The wave heights increase up to more than twice the incident wave height.
Udo Berger, Soren Kohlhase
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Numerical Analysis of Aerodynamic Interference of Two Passing Cylindrical Bodies at Supersonic Speeds [PDF]
مکانیک هوافضا, 2023 Aerodynamic interference is one of the phenomena that occurs when two flying objects pass near each other. In this case, the change in the pressure distribution on objects passing near each other causes a change in the aerodynamic forces.
Mohammad Ali Ranjbar +2 more
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Investigation on energy output structure of explosives near-ground explosion
Defence Technology, 2020 In order to give the energy output structure of typical explosives near-ground explosion in real ground conditions, the free-field shockwave, ground reflection shockwave and Mach wave overpressure time history of composition B explosive, RDX explosive ...
Wen-long Xu +4 more
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Particle Energization at a High Mach Number Perpendicular Shock: 1D Particle-in-cell Simulations
The Astrophysical Journal, 2023 In this paper, we use a 1D particle-in-cell simulation code to study particle preaccelerations at a high Mach number perpendicular shock. Our simulation results show that almost all of the injected particles can be reflected at the shock front, and then ...
Yufei Hao +6 more
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The theoretical basis of reservoir pressure in arteries. [PDF]
Exp PhysiolAbstract The separation of measured arterial pressure into a reservoir pressure and an excess pressure was introduced over 20 years ago as a heuristic hypothesis. Since then it has gained some traction through epidemiological studies that show that various measures of reservoir and excess pressure are independent risk factors for cardiovascular disease.
Parker KH, Hughes AD.
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Investigation of Flow Control for the Hypersonic Inlets via Counter Flow
International Journal of Aerospace Engineering, 2015 Experimental results show that there exist two flow fields in the hypersonic inlets when the forebody waves interact with the lip boundary, which is similar to the shock reflection ion hysteresis phenomenon.
Xiaoqiang Fan, Yuan Tao
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