Results 71 to 80 of about 385,605 (249)
Electronic Journal of Differential Equations, 2019 In this article, we consider the low Mach number limit of the compressible nematic liquid crystal flows in a 3D bounded domain. We establish the uniform estimates with respect to the Mach number for the strong solutions with large initial data in a ...
Boling Guo, Lan Zeng, Guoxi Ni
doaj
Jet-edge interaction tones [PDF]
, 2017 Motivated by the problem of jet-flap interaction noise, we study the tonal dynamics that occur when a sharp edge is placed in the hydrodynamic nearfield of an isothermal turbulent jet.
Agarwal, Anurag +6 more
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Ion acceleration in non-relativistic astrophysical shocks
, 2011 We explore the physics of shock evolution and particle acceleration in non-relativistic collisionless shocks using multidimensional hybrid simulations.
Gargaté, L., Spitkovsky, A.
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Noise suppression with high Mach number inlets [PDF]
Experimental results were obtained for two types of high Mach number inlets, one with a translating centerbody and a fixed geometry inlet (collapsing cowl) with no centerbody. The aerodynamic and acoustic performance of these inlets was examined.
Cherng, J. G., Lumsdaine, E., Tag, I.
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Theoretical and Applied Mechanics LettersThis study investigates the three-dimensional (3D) effects introduced by the end walls for an aspect ratio of 1 in ramp-induced shock wave boundary layer interactions.
Raja Mangalagiri, Satya P Jammy
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Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number [PDF]
An anechoic wind tunnel experiment was conducted to determine the effects of simulated flight on the noise characteristics of a high throat Mach number fan inlet.
Abbott, J. M. +2 more
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Measure-valued low Mach number limits of ideal fluids [PDF]
, 2021 Dennis Gallenmüller
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Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results [PDF]
The low frequency symmetric structural response and damping characteristics of the XB-70 airplane were measured at four flight conditions: heavyweight at a Mach number of 0.87 at an altitude of 7620 meters (25,000 feet); lightweight at a Mach number of 0.
Kordes, E. E. +2 more
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Electron Heating in High Mach Number Collisionless Shocks
Physical Review LettersThe energy partition in high Mach number collisionless shock waves is central to a wide range of high-energy astrophysical environments. We present a new theoretical model for electron heating that accounts for the energy exchange between electrons and ions at the shock.
A. Vanthieghem +5 more
openaire +5 more sources