Results 11 to 20 of about 16,981 (316)

Numerical simulation on effects of back pressure on supersonic condensation propertites of wet natural gas

open access: yesYou-qi chuyun, 2022
The back pressure at the outlet of supersonic cyclone separator usually causes aerodynamic shock wave in Laval nozzle, and the interaction of supersonic flow, shock wave and phase transition is very complicated.
Jiang BIAN   +6 more
doaj   +1 more source

Subsonic to Supersonic Nozzle Flows [PDF]

open access: yesSIAM Journal on Applied Mathematics, 2013
Steady, irrotational flow of a compressible fluid through a two-dimensional planar and axisymmetric nozzle is formulated and solved numerically in the hodograph or velocity plane. The Legendre potential is used to express the governing equation which for planar flow is linear and for axisymmetric flow nonlinear.
Kryeziu, O, Johnson, ER
openaire   +2 more sources

Reacting Flow Simulations of a Dual Throat-Dual Fuel Thruster

open access: yesJournal of Applied Fluid Mechanics, 2021
Numerical simulation of the supersonic turbulent reacting flow field in a dual throat- dual fuel rocket thrust chamber is presented. Future single stage to orbit and high lift space transportation missions aspire a reliable, efficient, and cost ...
S. Jayakrishnan, M. Deepu
doaj  

Research Progress of Microjet Control of Shock Wave/Boundary Layer Interactions in Supersonic Flow Field [PDF]

open access: yesHangkong bingqi, 2022
The phenomenon of shock wave/boundary layer interaction is inevitable in the supersonic flow field. The existence of this phenomenon will have a series of adverse effects on the inner and outer flow fields of the supersonic vehicle.
Xu Hao, Du Zhaobo, Zhong Xiangyu, Huang Wei
doaj   +1 more source

Thermoelastic stability of closed cylindrical shell in supersonic gas flow

open access: yesTheoretical and Applied Mechanics Letters, 2019
In this paper the problem of linear stability of a closed cylindrical shell under the action of both non-uniform temperature field and supersonic gas flow is considered.
G.Y. Baghdasaryan   +3 more
doaj   +1 more source

Characteristics of plasma flow profiles in a super-X-divertor-like configuration

open access: yesNuclear Materials and Energy, 2019
Plasma flow patterns in a super-X-divertor-like configuration are investigated by using a one-dimensional plasma fluid model with the anisotropic-ion pressure (AIP model).
Satoshi Togo   +9 more
doaj   +1 more source

Flow characteristics of sub- and supersonic jets issued from orifice and notched orifice nozzles, and application to ejector

open access: yesJournal of Fluid Science and Technology, 2019
The flow characteristics of sub- and supersonic under-expanded jets issued from circular nozzles have been studied well; however, this does not apply to sub- and supersonic jets from an orifice nozzle.
Toshihiko SHAKOUCHI   +3 more
doaj   +1 more source

An experimental investigation of a square supersonic jet and impinging jet on an inclined plate

open access: yesAIP Advances, 2020
Supersonic free jets and impinging jets are found in many engineering applications, such as short and vertical take-off and landing vehicles, cold gas dynamic spray processes, hot surface cooling mechanisms, and turbomachinery systems.
Thien Nguyen, Blake Maher, Yassin Hassan
doaj   +1 more source

Application of Prandtl’s Theory in the Design of an Experimental Chamber for Static Pressure Measurements

open access: yesSensors, 2021
Pumping in vacuum chambers is part of the field of environmental electron microscopy. These chambers are separated from each other by a small-diameter aperture that creates a critical flow in the supersonic flow regime.
Pavla Šabacká   +3 more
doaj   +1 more source

In-vitro study on apatite/titanium composite coatings with supersonic free-jet PVD

open access: yesScience and Engineering of Composite Materials, 2011
Hydroxyapatite (HAp) has many applications in the medical field. The objective of this study is to produce HAp/Ti composite coating with Supersonic Free-Jet PVD (SFJ-PVD).
Yumoto Atsushi   +4 more
doaj   +1 more source

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