Influence of Exhaust Nozzle Geometry on the Jet Potential Core Development

Daniel Eugeniu Crunteanu; Valentin Ionut Misirliu; Oana Dumitrescu; Bogdan Gherman

doi:10.4028/www.scientific.net/AMM.811.145

Paper Titles

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A Method to Increase the Natural Frequency of a Ground Moving System
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Global Analysis of Tip Clearance Influence on Centrifugal Compressor Performance
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Modeling and Simulation of a Hydroelectric Process
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Influence of Exhaust Nozzle Geometry on the Jet Potential Core Development
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On the Supersonic Combustion of Hydrogen around a Conical Obstacle Considering Variable Specific Heats with Application to Scramjets
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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 811Influence of Exhaust Nozzle Geometry on the Jet...

Influence of Exhaust Nozzle Geometry on the Jet Potential Core Development

Abstract:

In this paper, a numerical simulation was performed on a scale turbofan engine nozzle to asses the influence of two nozzle configurations over the flow performance while the nozzle is situated at a certain distance from the ground. The turbulence model chosen for this numerical simulation was SST k-ω to capture boundary layer detachment and jet attachment to the ground. For this analysis two different computational domains where considered, while for the third case, boundary conditions for secondary inlet where modified. To assess the impact of these geometry changes a comparison between cases is made at different location in the domain.

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Periodical:

Applied Mechanics and Materials (Volume 811)

Pages:

145-151

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.811.145

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Online since:

November 2015

Authors:

Daniel Eugeniu Crunteanu*, Valentin Ionut Misirliu, Oana Dumitrescu, Bogdan Gherman

Keywords:

CFD, Chevrons, Exhaust Nozzle, Hot Jet, Structured Grid, Turbulence

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