Results 41 to 50 of about 17,927 (212)

Study of axisymmetric underexpanded sonic jets with Mach disks (Density field measurements by rainbow schlieren deflectometry)

open access: yesNihon Kikai Gakkai ronbunshu, 2019
The underexpanded sonic jet issued from an axisymmetric convergent nozzle are experimentally investigated in which the nozzle is operated at a pressure ratio of 4.0 to produce a Mach disk in the jet plume.
Taishi TAKESHITA   +3 more
doaj   +1 more source

Investigation on Flow Characteristics of SVC Nozzles

open access: yesJournal of Applied Fluid Mechanics, 2018
Shock vectoring control (SVC) is an important method of fluidic thrust vectoring (FTV) for aero-engine exhaust system. It behaves better on nozzle of high pressure ratio, and is considered as an alternative TV technology for a future aero-engine with ...
S. H. I. Jingwei   +3 more
doaj  

Entrainment characteristics of unsteady subsonic jets [PDF]

open access: yes, 1979
The effectiveness of jet unsteadiness in enhancing flow entrainment was assessed. It was conducted that entrainment depends on the type and amount of jet unsteadiness.
Bremhorst, K.   +2 more
core   +1 more source

Transient, hypervelocity flow in an axisymmetric nozzle [PDF]

open access: yes29th Aerospace Sciences Meeting, 1991
The performance of an axisymmetric nozzle was examined which was designed to produce uniform, parallel flow with a nominal Mach number of 8. A free-piston driven shock tube was used to supply the nozzle with high-temperature, high-pressure test gas. Performance was assessed by measuring Pitot pressures across the exit plane of the nozzle and, over the ...
openaire   +1 more source

Recent advances in characterisation of subsonic axisymmetric nozzles [PDF]

open access: yesEPJ Web of Conferences, 2018
Nozzles are devices generating jets. They are widely used in fluidics and also in active control of flows past bodies. Being practically always a component of larger system, design and optimisation of the system needs characterisation of nozzle properties by an invariant quantity.
openaire   +4 more sources

Flow Feature in Supersonic Non-Isobaric Jet near the Nozzle Edge

open access: yesAerospace, 2022
Using the example of studying the supersonic underexpanded jet initial section, the issue of interpreting the experimental visualization data and Pitot pressure measurement data using the results of numerical calculations (2d RANS k-ω SST) is discussed ...
Valeriy Zapryagaev   +2 more
doaj   +1 more source

Three-dimensional full Euler flows in axisymmetric nozzles

open access: yesJournal of Differential Equations, 2013
Abstract In this paper, we consider global subsonic compressible flows through general infinitely long nozzles. The flow is governed by the steady full Euler equations. We find a new invariant along streamline. Take advantages of this, we reformulate the full Euler system into quasilinear second order equations of stream function.
Duan, Ben, Luo, Zhen
openaire   +2 more sources

Impinging Jet Resonant Modes at Mach 1.5 [PDF]

open access: yes, 2013
High speed impinging jets have been the focus of several studies owing to their practical application and resonance dominated flow-field. The current study focuses on the identification and visualization of the resonant modes at certain critical ...
Alvi, Farrukh, Davis, Timothy
core  

3-D axisymmetric subsonic flows with nonzero swirl for the compressible Euler-Poisson system [PDF]

open access: yes, 2016
We address the structural stability of 3-D axisymmetric subsonic flows with nonzero swirl for the steady compressible Euler-Poisson system in a cylinder supplemented with non small boundary data. A special Helmholtz decomposition of the velocity field is
Bae, Myoungjean, Weng, Shangkun
core   +2 more sources

Flow Structure of a Coaxial Circular Jet with Axisymmetric and Helical Instability Modes

open access: yesJournal of Fluid Science and Technology, 2011
The flow structures in a coaxial jet with axisymmetric and helical instability modes for a comparatively low Reynolds number were investigated. The flow visualization and the measurements of velocities were carried out in an open water tank. In addition,
Takahiro KIWATA   +4 more
doaj   +1 more source

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