Experimental Investigation of Nozzle Aspect Ratio Effects on Underexpanded Hydrogen Jet Release Characteristics

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ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (958 download)

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Book Synopsis Experimental Investigation of Nozzle Aspect Ratio Effects on Underexpanded Hydrogen Jet Release Characteristics by :

Download or read book Experimental Investigation of Nozzle Aspect Ratio Effects on Underexpanded Hydrogen Jet Release Characteristics written by and published by . This book was released on 2013 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Nozzle Geometry on Mixing Characteristics of Turbulent Free Orifice Jets

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (135 download)

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Book Synopsis Effect of Nozzle Geometry on Mixing Characteristics of Turbulent Free Orifice Jets by : Yaw Yeboah Afriyie

Download or read book Effect of Nozzle Geometry on Mixing Characteristics of Turbulent Free Orifice Jets written by Yaw Yeboah Afriyie and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted using particle image velocimetry to study the effect of nozzle geometry on turbulent free orifice jets. The nozzle geometries studied include the round, cross, flower, star, rectangular and elliptical nozzles (aspect ratio 2). The spread rate of the rectangular nozzle was 61% greater than the square nozzle while the elliptical nozzle was 45% greater than the round nozzle using the conventional half velocity width. The superior mixing capacity of the rectangular and elliptical nozzles is attributed to the axis-switching mechanism. Evaluation of the energy budget showed a higher level of production of turbulence and convection of the mean flow for the rectangular nozzle compared with the round nozzle. Two-point auto-correlation function revealed larger structures in the non-circular nozzles and in particular the rectangular nozzle. The Kolmogorov and Taylor microscales however, did not show any significant dependency on nozzle geometry.

An Experimental Investigation of Nozzle-exit Boundary Layers of Highly Heated Free Jets

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (142 download)

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Book Synopsis An Experimental Investigation of Nozzle-exit Boundary Layers of Highly Heated Free Jets by : Jan Lepicovsky

Download or read book An Experimental Investigation of Nozzle-exit Boundary Layers of Highly Heated Free Jets written by Jan Lepicovsky and published by . This book was released on 1990 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the effects of nozzle operating conditions on the development of nozzle-exit boundary layers of highly heated air free jets is reported in this paper. The total pressure measurements in the nozzle-exit boundary layer were obtained at a range of jet Mach numbers from 0.1 to 0.97 and jet total temperatures up to 900 K. The analysis of results shows that the nozzle-exit laminar boundary-layer development depends only on the nozzle-exit Reynolds number. For the nozzle-exit turbulent boundary layer, however, it appears that the effects of the jet total temperature on the boundary-layer integral characteristics are independent from the effect of the nozzle-exit Reynolds number. This surprising finding has not yet been reported. Further, laminar boundary-layer profiles were compared with the Pohlhausen solution for a flat-wall converging channel and an acceptable agreement was found only for low Reynolds numbers. For turbulent boundary layers, the dependence of the shape factor on relative Mach numbers at a distance of one momentum thickness from the nozzle wall resembles Spence's prediction. Finally, the calculated total pressure loss coefficient was found to depend on the nozzle-exit Reynolds number for the laminar nozzle-exit boundary layer, while for the turbulent exit boundary layer this coefficient appears to be constant.

GASFLOW-MPI: A Scalable Computational Fluid Dynamics Code for Gases, Aerosols and Combustion. Band 1 (Theory and Computational Model (Revision 1.0)

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Publisher : KIT Scientific Publishing
ISBN 13 : 3731504480
Total Pages : 124 pages
Book Rating : 4.7/5 (315 download)

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Book Synopsis GASFLOW-MPI: A Scalable Computational Fluid Dynamics Code for Gases, Aerosols and Combustion. Band 1 (Theory and Computational Model (Revision 1.0) by : Xiao, Jianjun

Download or read book GASFLOW-MPI: A Scalable Computational Fluid Dynamics Code for Gases, Aerosols and Combustion. Band 1 (Theory and Computational Model (Revision 1.0) written by Xiao, Jianjun and published by KIT Scientific Publishing. This book was released on 2016-04-06 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: Karlsruhe Institute of Technology (KIT) is developing the parallel computational fluid dynamics code GASFLOW-MPI as a best-estimate tool for predicting transport, mixing, and combustion of hydrogen and other gases in nuclear reactor containments and other facility buildings. GASFLOW-MPI is a finite-volume code based on proven computational fluid dynamics methodology that solves the compressible Navier-Stokes equations for three-dimensional volumes in Cartesian or cylindrical coordinates.

An Experimental Investigation of Highly Underexpanded Free Jets Impinging Upon a Parallel Flat Surface

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ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis An Experimental Investigation of Highly Underexpanded Free Jets Impinging Upon a Parallel Flat Surface by : Allen R. Vick

Download or read book An Experimental Investigation of Highly Underexpanded Free Jets Impinging Upon a Parallel Flat Surface written by Allen R. Vick and published by . This book was released on 1964 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Multi-component Jets Issuing from Model Pipeline Geometries with Application to Hydrogen Safety

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (119 download)

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Book Synopsis Experimental Investigation of Multi-component Jets Issuing from Model Pipeline Geometries with Application to Hydrogen Safety by : Majid Soleimani nia

Download or read book Experimental Investigation of Multi-component Jets Issuing from Model Pipeline Geometries with Application to Hydrogen Safety written by Majid Soleimani nia and published by . This book was released on 2018 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Development of modern safety standards for hydrogen storage infrastructure requires fundamental insight into the physics of buoyant gas dispersion into ambient air. Also, from a practical engineering stand-point, flow patterns and dispersion of gas originating from orifices in the side wall of circular pipe or storage tank need to be studied. In this thesis, novel configurations were considered to investigate the evolution of turbulent jets issuing from realistic pipeline geometries. First, the effect of jet densities and Reynolds numbers on vertical jets were investigated, as they emerged from the side wall of a circular pipe, through a round orifice. The resulting jet flow was thus issued through a curved surface from a source whose original velocity components were nearly perpendicular to the direction of the ensuing jets. Particle image velocimetry (PIV) and planar laser-induced fluorescence (PLIF) techniques were employed simultaneously to provide instantaneous and time-averaged flow fields of velocity and concentration. The realistic flow arrangement resulted in an asymmetric flow pattern and a significant deflection from the vertical axis of jets. The deflection was influenced by buoyancy, where heavier gases deflected more than lighter gases. These realistic jets experienced faster velocity decay, and asymmetric jet spreading compared to round jets due to significant turbulent mixing in their near field. In addition to that, horizontal multi-component jets issuing from a round orifice on the side wall of a circular tube were also investigated experimentally by the means of simultaneous velocity and concentration measurements. A range of Reynolds numbers and gas densities were considered to study the effects of buoyancy and asymmetry on the resulting flow structure. The realistic pipeline jets were always exhibited an asymmetry structure and found to deflect about the jet's streamwise axis in the near field. In the far field, the buoyancy dominated much closer to the orifice than expected in the axisymmetric round jet due to the realistic leak geometry along with the pipeline orientation considered in this study. In general, significant differences were found between the centreline trajectory, spreading rate, and velocity decay of conventional horizontal round axisymmetric jets issuing through flat plates and the pipeline leak-representative jets considered in the present study. Finally, the dispersion of turbulent multi-component jets issuing from high-aspect-ratio slots on the side wall of a circular tube were studies experimentally by employing simultaneous PIV and PLIF techniques. Two transversal & longitudinal oblong geometries in respect to the longitudinal axes of the tube , and with an aspect ratio of 10 were considered in this study. Both horizontal and vertical orientations along with broad range of Reynolds numbers and gas densities were considered to investigate the effects of buoyancy and asymmetry on the resulting flow structure. The ensuing jets were found to deflect along the jet streamwise axis, once more, due to the realistic pipeline leak-representative configuration. It was also found that increases in aspect ratio of these realistic jets caused a reduction in the angle of deflection, jet centreline decay rates and the width growth on both velocity and scalar fields compared to their round jets counterparts, most notably in the far field. These findings indicate that conventional jets (those that are issuing through flat surfaces) assumptions are inadequate to predict gas concentration, entrainment rates and, consequently, the extent of the flammability envelope of realistic gas leaks. Thus, extreme caution is required when using conventional jet assumptions to describe the physics of a buoyant jet emitted from realistic geometries.

Experimental Investigation of Secondary Jets from Two-dimensional Nozzles with Various Exit Mach Numbers for Hypersonic Control Application

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ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Investigation of Secondary Jets from Two-dimensional Nozzles with Various Exit Mach Numbers for Hypersonic Control Application by :

Download or read book Experimental Investigation of Secondary Jets from Two-dimensional Nozzles with Various Exit Mach Numbers for Hypersonic Control Application written by and published by . This book was released on 1967 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Influence of Nozzle-flow Properties on the Primary Spray Breakup

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ISBN 13 : 9783832290016
Total Pages : 143 pages
Book Rating : 4.2/5 (9 download)

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Book Synopsis Experimental Investigation of the Influence of Nozzle-flow Properties on the Primary Spray Breakup by : Benjamin Sebastian Balewski

Download or read book Experimental Investigation of the Influence of Nozzle-flow Properties on the Primary Spray Breakup written by Benjamin Sebastian Balewski and published by . This book was released on 2010 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 964 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1988 with total page 964 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

An Investigation of the Effect of an Adjacent Surface on an Underexpanded Jet Discharging from a Two-dimensional Nozzle at Sonic Velocity

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ISBN 13 :
Total Pages : 192 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis An Investigation of the Effect of an Adjacent Surface on an Underexpanded Jet Discharging from a Two-dimensional Nozzle at Sonic Velocity by : Mordecai Philip Rodd

Download or read book An Investigation of the Effect of an Adjacent Surface on an Underexpanded Jet Discharging from a Two-dimensional Nozzle at Sonic Velocity written by Mordecai Philip Rodd and published by . This book was released on 1964 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical Investigation Of Hydrogen Under-Expanded Jet Flow Considering Viscous Effects

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ISBN 13 :
Total Pages : 100 pages
Book Rating : 4.:/5 (113 download)

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Book Synopsis Numerical Investigation Of Hydrogen Under-Expanded Jet Flow Considering Viscous Effects by : Farbid Vakilimoghaddam

Download or read book Numerical Investigation Of Hydrogen Under-Expanded Jet Flow Considering Viscous Effects written by Farbid Vakilimoghaddam and published by . This book was released on 2017 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt: Hydrogen is the simplest and the most plentiful element in the universe. It is the cleanest burning fuel with water as the only by-product of the combustion process. Nevertheless, the low energy density per volume of hydrogen requires highly pressurized tanks to store a reasonable amount of energy. Highly pressurized storage tanks increase the risk of tank valve failure and hydrogen release into atmosphere.In this study, two approaches are developed to investigate sudden hydrogen release. In the first approach, an analytical method is used to analyze the time histories of stagnation properties inside the chamber and sonic properties at the throat. In the second approach, computational fluid dynamics (CFD) analysis is conducted using Ansys CFX solver. Unsteady 3D Navier-Stokes equations along with an additional transport equation are the governing equations of the flow. This CFD analysis is second order accurate in time and space. The SST k-} turbulence model is employed to study the turbulent properties of the flow. Peng-Robinson real gas EOS is used for the accurate prediction of the hydrogen properties. A fully structured high quality mesh is constructed with.

Experimental Investigation of the Effect of Inlet Geometry on a Fluidic Power Nozzle

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ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.:/5 (24 download)

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Book Synopsis Experimental Investigation of the Effect of Inlet Geometry on a Fluidic Power Nozzle by : Laurence Lee Losh

Download or read book Experimental Investigation of the Effect of Inlet Geometry on a Fluidic Power Nozzle written by Laurence Lee Losh and published by . This book was released on 1971 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Characteristics of the Airflow in a Mach 10 Hypersonic Nozzle

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ISBN 13 :
Total Pages : 58 pages
Book Rating : 4.:/5 (115 download)

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Book Synopsis Experimental Investigation of the Characteristics of the Airflow in a Mach 10 Hypersonic Nozzle by : Azzedine Missoum

Download or read book Experimental Investigation of the Characteristics of the Airflow in a Mach 10 Hypersonic Nozzle written by Azzedine Missoum and published by . This book was released on 1986 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental and Numerical Investigation of the Ozone Addition Effect on Ignition Characteristics of Hydrogen-jet Fuel in a Constant-volume Combustion Chamber

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (136 download)

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Book Synopsis Experimental and Numerical Investigation of the Ozone Addition Effect on Ignition Characteristics of Hydrogen-jet Fuel in a Constant-volume Combustion Chamber by :

Download or read book Experimental and Numerical Investigation of the Ozone Addition Effect on Ignition Characteristics of Hydrogen-jet Fuel in a Constant-volume Combustion Chamber written by and published by . This book was released on 2022 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 654 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1992 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Experimental Investigation of the Effect of Chamber Length on Jet Precession

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (658 download)

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Book Synopsis The Experimental Investigation of the Effect of Chamber Length on Jet Precession by : Adam Martin Madej

Download or read book The Experimental Investigation of the Effect of Chamber Length on Jet Precession written by Adam Martin Madej and published by . This book was released on 2010 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Pulsed Jet Nozzle Blowing for Forebody Flow Control

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Experimental Investigation of Pulsed Jet Nozzle Blowing for Forebody Flow Control by : Jennifer L. Sedor

Download or read book Experimental Investigation of Pulsed Jet Nozzle Blowing for Forebody Flow Control written by Jennifer L. Sedor and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: