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Supersonic mixing layer

WebNov 2, 2024 · A supersonic mixing layer at a convective Mach number of 0.8 was investigated by large eddy simulation. Turbulent structures and statistics of the mixing layer interacting with an oblique shock at different strengths in the self-preserving stage were investigated and compared with the shock-free mixing layer. An inflection point … WebSep 12, 2002 · Direct numerical simulation is used to investigate three-dimensional temporal supersonic mixing layers at two convective Mach numbers 1.2 and 1.6. At the convective …

MHz rate flow visualization of the evolution of supersonic …

WebPublished: June 29, 2010 Abstract The distorted wavefront due to the density fluctuation of the supersonic mixing layer is measured by the nano-based planar laser scattering technique, with the spatiotemporal resolutions as 10 − 1 mm and 1 μs (time interval between two exposures), respectively. WebApr 28, 2024 · Among such points are problems in the hydrodynamic instability of supersonic shear flows (boundary layer and mixing layer), the development of small perturbations and their interaction with compression shocks, the mechanisms of acoustic emission by high-speed flows, the emergence of self-oscillations, and the shock-wave … kew road southport https://combustiondesignsinc.com

The spatial growth of supersonic reacting mixing layers: …

WebMar 29, 2006 · Abstract. Plane turbulent mixing between two streams of different gases (especially nitrogen and helium) was studied in a novel apparatus. Spark shadow pictures … WebExperiments were conducted in a two-stream planar mixing layer at convective Mach numbers, Mc, of 0.28, 0.42, 0.50, 0.62 and 0.79. Planar laser Mie scattering (PLMS) from a … WebJan 1, 2024 · In this paper, supersonic mixing layers with various splitter plate thicknesses are simulated. The main purpose of this numerical paper is to investigate the roles of the … kewr procedures

Large-scale structure and entrainment in the supersonic mixing layer J…

Category:Evolution characteristics of subsonic-supersonic mixing …

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Supersonic mixing layer

Flow visualization of the large-scale structures in supersonic …

WebAug 31, 2016 · One of the main difficulties in the simulation of compressible flows is how to distinguish the discontinuities which may widely exist in supersonic flows. Jiang and Shu [ 12] proposed the weighted essentially non-oscillatory (WENO) scheme to capture shock waves with almost no oscillations. WebDec 1, 2024 · The remarkable feature of the subsonic-supersonic shear mixed flow is its strong compressibility. The shear mixing flow was first studied on the low-speed …

Supersonic mixing layer

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WebMay 28, 2024 · The supersonic mixing layer is a common compressible turbulent flow, which exists in supersonic ejectors and combined cycle engines. Taking a rocket-based … WebApr 11, 2024 · The current study aims to reveal how the pressure gradient acts on the subsonic–supersonic mixing layer, the wave structure caused by a pressure gradient, and …

WebMar 9, 2024 · The study of the turbulent supersonic particle-laden mixing layers flows is considered as one of the perspective ways of improving mixing of fuel and oxidant and consequently of the combustion. WebMay 17, 2012 · Mixing enhancement for supersonic mixing layer by using plasma synthetic jet. Acta Physica Sinica, Vol. 68, No. 17. Direct numerical simulation of subsonic–supersonic mixing layer. Acta Astronautica, Vol. 153. Visual hull based 3D reconstruction of shocks in under-expanded supersonic bevelled jets.

WebMay 28, 2024 · The supersonic mixing layer is a common compressible turbulent flow, which exists in supersonic ejectors and combined cycle engines. Taking a rocket-based combined cycle engine (RBCC) as an … WebFeb 15, 2024 · This difference is explained by the presence of a certain level of turbulence in the mixing layer of the real jet, as compared to the completely laminar model implied in the computations. The supersonic core lengths calculated from the experimental data obtained by the Pitot tubes with diameters up to 1.1/0.8 mm coincide with each other.

WebApr 11, 2024 · To summarize, the high-temporal-resolution evolution of the subsonic–supersonic mixing layers and the flow characteristics caused by pressure gradients, such as shock waves, expansion waves, and reflected shocks, were investigated via a high-speed schlieren system. The compressible mixing layer deflects to the lower …

WebDec 1, 2024 · A supersonic–subsonic mixing flow is an unsteady flow. A subsonic reverse flow zone significantly influences the stability of a numerical calculation and is generated … kewron beach storeWebMay 16, 2024 · Cao W., Zhou H., Existence of shocklets in a two-dimensional supersonic mixing layer and its influence on the flow structure. Science in China, Series A, 2001, 44(9): 1182–1188. Article MATH ADS Google Scholar Download references. Acknowledgement. This work was supported by the National Natural Science Foundation of China (51805453 … is johnson and johnson safestWebA new computer program has been written to calculate the properties of the recirculating base flow region of a rocket exhaust plume. The nozzle stream and the freestream, either of which may be supersonic, mix turbulently to form an axisymmetric compressible free boundary layer. Solutions of the elliptic differential equations, which incorporate a two … kewr united terminalWebAug 17, 2024 · The supersonic mixing layer is significantly anisotropic, and the streamwise turbulent intensity is larger than the transverse and spanwise turbulent intensities. The non-isothermal effects enhance the energy transfer from the streamwise Reynolds stress to transverse and spanwise Reynolds stresses in the initial shear layer, and the mixing ... is johnson and johnson safe for kidsWebApr 1, 2024 · A supersonic mixing layer at a convective Mach number of 0.8 was investigated by large eddy simulation. Turbulent structures and statistics of the mixing layer interacting with an oblique shock at ... is johnson an irish nameWebFor supersonic mixing-layers, Eq. (6.8) does not correctly describe the spreading rate. This is illustrated in Figure 6.12, where measured spreading rates in supersonic backward facing steps are plotted versus the corresponding density ratio … is johnson and johnson safe for women over 50WebApr 26, 2006 · An experiment in a supersonic mixing layer at convective Mach number M c = 0.62 was performed to study the evolution of a flow from a turbulent boundary layer to a … kewr scenery msfs