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Accretion of the Vlasov gas onto a Kerr black hole: Wolfram Mathematica notebooks
Wolfram Mathematica notebooks supplementing the articles: Patryk Mach, Mehrab Momennia, Olivier Sarbach, Accretion of a Vlasov gas by a Kerr black hole, arXiv:2508.04783 (2025); Patryk Mach, Mehrab Momennia, Olivier Sarbach, Bondi-type accretion onto a ...
Mehrab Momennia +2 more
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Mach number dependence of electron heating in high Mach number quasiperpendicular shocks
The efficiency of electron heating through microinstabilities generated in the transition region of a quasiperpendicular shock for a wide range of Mach numbers is investigated by utilizing particle-in-cell PIC simulation and model analyses. In the model analyses saturation levels of effective electron temperature as a result of microinstabilities are ...
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Estimation of Drag divergence Mach number for General Transport wing
Drag divergence Mach number plays a major role to decide the maximum operating speed without a severe drag penalty for high speed subsonic civilian aircraft.
Dhanalakshmi, K +2 more
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Strategic Analysis of MACH MOTORS s.r.o.
This bachelor’s thesis focuses on the strategic analysis of MACH MOTORS s.r.o., a company operating in the field of car and motorcycle sales and serving as an authorized dealer of several major brands.
Mach, Lubomír
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Measurements of the Mach number in a Plasma Flow by a Four-tip Mach Probe
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Detonation Wave Mach Number Dependence in a High Mach Number Flows
The paper presents a study of detonation propagation in supersonic crossflows over a range of Mach numbers. The work is focused on characterizing the detonation wave dependence on the supersonic cross-stream Mach number. A high-enthalpy combustor is used to provide continuous premixed supersonic crossflows that interact with an orthogonal detonation ...
Sosa, Jonathan +2 more
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Shock-Vortex Interactions at High Mach Numbers
Journal of Scientific Computing, 2003zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Audrey Rault +2 more
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On vortex sound at low Mach number
Journal of Fluid Mechanics, 1978A transformation is described which relates the sound generated by low Mach number flow to the flow vorticity. For compact flow fields the apparent sound source is of quadrupole type and linear in the vorticity and therefore also linear in the flow velocity.
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Mach number and temperature effects on jets
11th Fluid and PlasmaDynamics Conference, 1978M were carried out in a round jet over a range of exit Mach numbers from 0.3 to 1.7 and exit-toambient temperature ratios of 0.8 to 2.3 using a laser velocimeter. Mean velocities and turbulence intensities were measured and their distributions in the radial and axial directions were obtained.
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