fluent software research papers
CFD Analysis of Conical Nozzle for Mach 3 at Various Angles of Divergence withFluent Software
free download
ABSTRACT Numerical study has been conducted to understand the gas flows in a conical nozzle at different degree of angle using 2 dimensional axi-symmetric models, which solves the governing equations by a control volume method. The nozzle geometry co-ordinates
Prediction of natural convection in an air-filled cubical cavity usingFLUENT Software
free download
shows a comparison between the average Nusselt number on the hot and cold surfaces and the experimentally measured values on the cold surface, percentage of errors, defined as (NuNum–NuExp)/NuExpx100, as well as the highest residuals for the
CFD Analysis of a Hydrogen Fueled Mixture in Scramjet Combustor with a Strut Injector by UsingFluent Software
free download
ABSTRACT In this study, k-e model has been used to examine supersonic flow in a model scramjet combustor. The configuration used is similar to the DLR (German Aerospace Center) scramjet model and it is consists of a one-sided divergent channel with a wedge-
Effects of Variation of Specific Heat on Temperature in Gaseous Combustion withFluent Software
free download
ABSTRACT The combustion is modeled using one-step reaction mechanism assuming complete conversion of the fuel to CO2 and H2O. This analysis illustrates the important role of the heat capacity in the prediction of peak flame temperature. The use of a constant Cp
CFD Analysis of Four Jet Flow at Mach 1.74 withFluent Software
free download
ABSTRACT The variations in mean velocity profiles of the x component along x-axis of the four jets at the designed Mach number is discussed in this research paper. It is found that the velocity profiles are fairly symmetrical about y= 0. The velocities and its gradients decay
CFD analysis of twin jet flow at Mach 1.74 withfluent software
free download
ABSTRACT The variations in mean velocity profiles of the x component along x-axis of the twin jets at the designed Mach number is discussed in this research paper. The variations in mean velocity profiles of the x component along x-axis of the twin jets at B= 9 and Me 1.74
Challenges in realizing vascular fluid-structure-interaction usingFluentand Abaqussoftware
free download
ABSTRACT We established a fluid-structure interaction (FSI) coupling between the fluid-solver fluent6.2 (Fluent, Inc.) and the structural solver abaqus 6.5 (Abaqus, Inc.). Two FSI-coupling schemes were established. For the first scheme an Aitkin-like acceleration was used to
Technology in Engineering Education: UsingFLUENT Softwareto Evaluate and Solve Computational Fluid Dynamics Problems
free download
ABSTRACT The introduction of computationalsoftwarehas revolutionized the engineering profession. The increased dependency on this type ofsoftwarein the engineering profession has proposed an increase in efficiency within the industry. As a result, new
Study the Effects of Bridge Pier Shape on the Flow Pattern Using theFluent Software
free download
ABSTRACT In this paper, the 3-D flow pattern around the pier with different sections is simulated usingFluent software. The pier sections modeled in this study included circular, spindle, oval, rectangular, square, and combined (rectangle-circle) sections. Thesoftwaresolves
COMPARISON OF FLOW ANALYSIS OF A SUDDEN AND GRADUAL CHANGE OF PIPE DIAMETER USINGFLUENT SOFTWARE
free download
ABSTRACT This paper describes an analytical approach to describe the areas where Pipes (used for flow of fluids) are mostly susceptible to damage and tries to visualize the flow behaviour in various geometric conditions of a pipe.Fluent softwarewas used to plot the
CFD Analysis of Mixing and Combustion of a Hydrogen Fueled Scramjet Combustor with a Strut Injector by UsingFluent Software
free download
ABSTRACT A numerical study of combustion enhancement has been performed for a Mach 2 model scramjet (supersonic combustion ramjet) combustor. The configuration used is similar to the DLR (German Aerospace Center) scramjet model and it is consists of a one-sided
CFD Analysis of Twin Jet Supersonic Flow withFluent Software
free download
ABSTRACT Supersonic flows associated with missiles, aircraft, missile engine intake and rocket nozzles are often steady. The shape of the nozzle geometry is increasingly attractive in heating, ventilation and air conditioning applications. The objective of the present work
EASy!™ for Pumps DesignSoftwareUsesFluentTechnology
free download
V Stage - DynamicMesh - mesco.com.pl Fluent'spartner in turbomachinery designsoftware, Concepts NREC, has announced the release of their new EASy! for Pumpssoftware. EASy! for Pumps provides designers with a complete system for the design of pump flow paths including impellers, diffusers, and
Use ofFLUENT Softwarein a First-Year Engineering Microfluidic Design Course
free download
ABSTRACT Currently, the integration of computational fluid dynamics (CFD)softwareis typically only seen in higher level courses at the undergraduate level(1)(2)(3). In this case, students are equipped with the basics of fluid dynamics from their core classes, which allows them
PERFORMANCE ANALYSIS AND CALCULATION OF DIFFERENT PARAMETERS OF CONDENSER USING ANSYSFLUENT SOFTWARE
free download
RM Gupta, S Singh, MS Srivastava - ijaiem.org ABSTRACT Modern era is the era of science and technology; here the things are changing very rapidly. Modern technology has advances the things. It has made the things easier and provided a comfort to humankind. The condenser is a heat-transfer device. It is used to
Fire Study of Melting Fiberglass UsingFLUENTCFDSoftware
free download
SG Rochelle, GS Whittaker, MJ Maness, JW Chastain - 2010 - allriskengineering.com ABSTRACT Thermal insulation is used in chemical plants primarily as a tool to prevent energy loss. However, when properly designed it provides the added benefit of allowing smaller relief valves to be used when designing relief systems in the fire case.
SIMULATION OF A FLOW AROUND A WEDGE-SHAPED BODY USINGFLUENTCFDSOFTWARE
free download
Analysis of literature has revealed an interest in manned aircraft which operate in the low hypersonic flight regime at approximately Mach 6 or at even higher hypersonic speeds [1-5]. If a manned aircraft has no escape systems any more or less serious accident could result
-SOFTWARE SALES SERVICE-https://www.engpaper.net--