Results 11 to 20 of about 4,553 (269)
Thermoelastic stability of closed cylindrical shell in supersonic gas flow
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
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
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
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]
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
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
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
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
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
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

