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[PDF] Top 20 Numerical and Experimental Invetigations of the Nozzle Geometry in Supersonic Mixing.

Has 10000 "Numerical and Experimental Invetigations of the Nozzle Geometry in Supersonic Mixing." found on our website. Below are the top 20 most common "Numerical and Experimental Invetigations of the Nozzle Geometry in Supersonic Mixing.".

Numerical and Experimental Invetigations of the Nozzle Geometry in Supersonic Mixing.

Numerical and Experimental Invetigations of the Nozzle Geometry in Supersonic Mixing.

... poor mixing with conical nozzle. The mixing between the two streams is the result of only the shear layer interaction between streams in conical configuration whereas in Oval configuration ... See full document

8

Numerical Simulation of Supersonic Overexpanded Jet from 2-D Convergent-Divergent Nozzle

Numerical Simulation of Supersonic Overexpanded Jet from 2-D Convergent-Divergent Nozzle

... the mixing extent and simulation of the Mach ...convergent-divergent nozzle, at overexpansion and near correct-expansion conditions (correct expansion for Mach ...the experimental results of Shantanu ... See full document

7

Preliminary study of the primary nozzle position of a supersonic air ejector with a constant-area mixing chamber

Preliminary study of the primary nozzle position of a supersonic air ejector with a constant-area mixing chamber

... The numerical results obtained on 2D axisymmetric models have been ...the experimental data shows some discrepancies, particularly in the off-design ...simplified numerical models or by other ... See full document

6

Effects of Supersonic Nozzle Geometry on Characteristics of Shock Wave Structure

Effects of Supersonic Nozzle Geometry on Characteristics of Shock Wave Structure

... and experimental researches on the sym- metric and asymmetric shock wave system in a planar nozzle were presented by Xiao et ...the nozzle exit to cross- sectional area at the nozzle ...of ... See full document

6

Effects of Nozzle Lip Length on Reduction of Transonic Resonance in 2D Supersonic Nozzle

Effects of Nozzle Lip Length on Reduction of Transonic Resonance in 2D Supersonic Nozzle

... as supersonic air- craft engine, jet propulsion thrust vectoring, fuel injec- tion for supersonic combustion, soot blower devices, thermal spray devices, ...the supersonic jet noise consists of three ... See full document

6

Experimental and Numerical Study on Supersonic Ejectors Working with R-1234ze(E)

Experimental and Numerical Study on Supersonic Ejectors Working with R-1234ze(E)

... primary nozzle operates in the over-expanded regime in both cases the ideal and the real gas model, because the jet of the primary stream is slightly converged toward the ejector centre and a complex pattern of ... See full document

10

Measurement and calculating of supersonic ejectors

Measurement and calculating of supersonic ejectors

... with numerical and experimental investigation of the flow in an air to air supersonic ejector with constant area mixing ...The mixing chamber of previous ejector was completely repaired ... See full document

7

Mixing, Chemical Reactions, and Combustion in Supersonic
Flows

Mixing, Chemical Reactions, and Combustion in Supersonic Flows

... Simulating supersonic combustion has its own ...of supersonic combustors through direct numerical simulation (DNS) is not currently feasible, nor anticipated in the foreseeable ... See full document

156

Numerical and Experimental Studies of Mixing of High Temperature Critical Water

Numerical and Experimental Studies of Mixing of High Temperature Critical Water

... flow pattern were observed using temperature fields. The general purpose three-dimensional CFD package FLUENT was used to solve the governing equations. A three- dimensional numerical model representing as Fig 1 ... See full document

5

Numerical and Experimental Investigation of Motor Pressure Effect on Thermochemical Erosion of Graphite Nozzle in Solid Fuel Engines

Numerical and Experimental Investigation of Motor Pressure Effect on Thermochemical Erosion of Graphite Nozzle in Solid Fuel Engines

... the nozzle for different pressures is shown in Figure ...the nozzle throat for 300 and 500 bars pressure, it can be seen that the pressure increases by 66 percent, where as erosion rate can vary by 100 ... See full document

9

Turbulent mixing layer experiment in supersonic flow

Turbulent mixing layer experiment in supersonic flow

... confined to determine the mean velocity profiles and the rates of growth of the free mixing layer by direct Pitot pressure measurements Maydew and Reed 1 and Johannesen 2» or density dis[r] ... See full document

229

Experimental measurement and numerical modeling of cavitating flow in converging-diverging nozzle

Experimental measurement and numerical modeling of cavitating flow in converging-diverging nozzle

... Another batch of simulations focused on higher flow rates (10,28 and 13 l/s). No reliable velocity measurements were obtained for those regimes, because caviting phase was present in the centre of the CD nozzle. ... See full document

8

Design of a test facility for probe calibration

Design of a test facility for probe calibration

... The above presented method for design of a nozzle as- sumes an inviscid flow. However, as was already men- tioned, the real situation must deal with boundary layers which influence the effective cross-section. From ... See full document

8

Design of Minimum Length Supersonic Nozzle using the Method of Characteristics

Design of Minimum Length Supersonic Nozzle using the Method of Characteristics

... A nozzle is a device designed to control the characteristics like pressure, velocity, density ...A nozzle is often a pipe or tube of varying cross sectional area and it can be used to direct or modify the ... See full document

5

Designing and prototyping a small scale steam driven jet pump

Designing and prototyping a small scale steam driven jet pump

... Like stated above the steam driven jet pump was at first designed to feed large locomotive boilers. Although it has been researched thoroughly through- out the years and large scale SDJP’s are frequent deployed on big ... See full document

73

Nearshore mixing due to the effects of waves and currents

Nearshore mixing due to the effects of waves and currents

... deviation of velocity from the depth averaged velocity. For the steady turbulent flow without any waves, the longitudinal shear dispersion and the turbulent diffusion coefficients have been studied by Elder (1959), Holly ... See full document

307

Experimental and numerical analyses of the cavitational flows around a hydrofoil

Experimental and numerical analyses of the cavitational flows around a hydrofoil

... The intensive development of measuring methods and the large number of experimental re- sults available, has enabled the numerical modelling of cavitational flows. The models are based on multi- phase-flow ... See full document

16

Movement Analysis of a Fluid through a Laval Nozzle Axial Symmetry with Fluent Program

Movement Analysis of a Fluid through a Laval Nozzle Axial Symmetry with Fluent Program

... The purpose of the paper is to present the form of partial differential equations in analysis of usage for the transition from subsonic to supersonic by Laval nozzle and using Fluent program to determine ... See full document

12

Effects of injection nozzle configuration on secondary injection into supersonic flow

Effects of injection nozzle configuration on secondary injection into supersonic flow

... D ata consisted of static pre ssure measurements on the wall near the inj e cto r , total pres sure prof iles in the wake of the injectant plume , and concentration measurements downstre[r] ... See full document

59

Numerical and Experimental Study of the Trichel Pulses in Needle-plane Geometry

Numerical and Experimental Study of the Trichel Pulses in Needle-plane Geometry

... an experimental study of the negative corona discharge in a needle-plane geometry are reported in this ...The experimental data were compared with the results of a series of numerical ... See full document

127

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