Results 11 to 20 of about 4,553 (269)

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

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

Supersonic flow control [PDF]

open access: yesShock Waves, 2015
Shock wave-induced boundary layer interactions are unavoidable in high-speed flows. The strong adverse pressure gradient imposed by the shock on the incoming undisturbed boundary layer may result in flow separation that is associated with low-frequency oscillations of the separation shock.
Verma, S., Hadjadj, Abdellah
openaire   +3 more sources

Numerical research on flow field starting of supersonic compressor in outlet-opening wind tunnel

open access: yesHangkong gongcheng jinzhan
The process from test starting to supersonic flow state established in an outlet-opening wind tunnel,i. e. the starting problem of supersonic flow,has become a recognized challenge.
ZHANG Tianlong   +4 more
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

Supersonic micro-jet of straight micro-tube exit

open access: yesJournal of Thermal Science and Technology, 2015
The experimental investigations on the phenomenon of supersonic flow at the exit of straight micro-tubes with diameters ranging from 150 to 530 μm were conducted.
Chungpyo HONG   +4 more
doaj   +1 more source

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