Relevant bibliographies by topics / Supersonic flows

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Academic literature on the topic 'Supersonic flows'

Author: Grafiati
Published: 6 September 2023

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Journal articles on the topic "Supersonic flows"

1

Uskov, Vladimir I. "Asymptotic solution of the Cauchy problem for the first-order equation with perturbed Fredholm operator". Russian Universities Reports. Mathematics, № 129 (2020): 48–56. http://dx.doi.org/10.20310/2686-9667-2020-25-129-48-56.

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We consider the Cauchy problem for a first-order differentialequation in a Banach space. The equation contains a small parameter in the highest derivative and a Fredholm operator perturbed by an operator addition on the right-hand side. Systems with small parameter in the highest derivative describe the motion of a viscous flow, the behavior of thin and flexible plates and shells, the process of a supersonic viscous gas flow around a blunt body, etc. The presence of a boundary layer phenomenon is revealed; in this case, even a small additive has a strong influence on the behavior of the solution. As
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Huynh, Juliette, Frédéric Hébert, Pierre-Elie Larré та Mathias Albert. "Stationary transport above the critical velocity in a one-dimensional superflow past an obstacle". Europhysics Letters, 17 серпня 2023. http://dx.doi.org/10.1209/0295-5075/acf15a.

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Abstract We consider in this work the different possible stationary flows of a one dimensional quantum fluid in the mean-field regime. We focus on the supersonic regime where a transition from a time dependent flow to a stationary diffractive flow occurs at a given critical velocity.
We give nonperturbative results for this critical velocity in the presence of a localised obstacle of arbitrary size and strength. In addition, we discuss the existence of superfluid-like solution in the supersonic regime due to resonant transport and provide a complete map of the different regimes of stationary tr
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3

Pascale, Ash, Trevor Lafleur, and Cormac S. Corr. "Bidirectional Vortex Stabilization of a Supersonic Inductively Coupled Plasma Torch." Journal of Physics D: Applied Physics, February 13, 2023. http://dx.doi.org/10.1088/1361-6463/acbb8a.

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Abstract Radio-frequency (RF) inductively coupled plasma (ICP) torches using a supersonic nozzle have many industrial materials processing applications and have also been proposed as novel electrothermal plasma thrusters for space propulsion. The gas injection method in plasma torches plays an important role in both gas heating dynamics and overall discharge stabilization. Here, we investigate reverse vortex gas injection into a supersonic ICP torch for RF powers up to 1 kW, argon mass flow rates between 15-180 mg/s, and plasma torch pressures from 270 Pa to 50 kPa. In this configuration, gas is
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4

Dave, Shreyansh S., Oindrila Ganguly, P. S. Saumia та Ajit Mohan Srivastava. "Hawking radiation from acoustic black holes in hydrodynamic flow of electrons". Europhysics Letters, 29 серпня 2022. http://dx.doi.org/10.1209/0295-5075/ac8d71.

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Abstract Acoustic black holes are formed when a fluid flowing with subsonic velocities, accelerates and becomes supersonic. When the flow is directed from the subsonic to supersonic region, the surface on which the normal component of fluid velocity equals the local speed of sound acts as an acoustic horizon. This is because no acoustic perturbation from the supersonic region can cross it to reach the subsonic part of the fluid. One can show that if the fluid velocity is locally irrotational, the field equations for acoustic perturbations of the velocity potential are identical to that of a massless
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Dissertations / Theses on the topic "Supersonic flows"

1

Singh, Vishal. "Spray Interaction with Supersonic Crossflow." Thesis, 2021. https://etd.iisc.ac.in/handle/2005/5438.

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The flow residence time in a scramjet combustor is of the order of a millisecond (10−3s). High energy density liquid fuels are the energy carriers of choice in scramjet engines, however liquid fuels must be atomized, evaporated and mixed before heat release by combustion can occur. Atomization, mixing and ignition require fnite time. Therefore it is important to study spray formation and its atomization in supersonic flows. Experiments are performed to study the spray formation from a water jet injected through a plain orifce atomizer with an exit diameter (d) of 1 mm, into a Mach 2.2 super
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