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Paper Title
AERODYNAMIC STUDY OF FLOW THROUGH CONVERGENT-DIVERGENT NOZZLE AND STUDY OF VARIOUS PARAMETERS BY USING ANSYS15.0
Authors
Shakeel Ahmad, Devesh Kumar
Keywords
Bell type nozzle, CFD, Numerical Analysis, Reynolds number.
Abstract
In this paper, we have been to analyses two bell nozzles of varying length and a similar cone nozzle, with the
same exit area ratio. By running these nozzle configurations under similar conditions at different altitudes, the
velocity and pressure contours are obtained. By studying these contours, it is found that the 85% Bell Nozzle
runs at design conditions over a greater range of altitude than the Cone Nozzle. Also below 70% Bell Nozzle
length, it is found that the exhaust gas flow becomes highly unstable and the thrust produced is very low. On
calculating the specific impulses for each condition, it is found that the 85% Bell Nozzle has a 6-7% loss when
compared to the cone Nozzle. The k- model with standard wall treatment was used for analyzing the flow. Here
the working fluid has been taken as air. All the calculations were done by using ANSYS-15.0 Workbench.
IJCRT's Publication Details
Unique Identification Number - IJCRT2109072
Paper ID - 211392
Page Number(s) - a589-a597
Pubished in - Volume 9 | Issue 9 | September 2021
DOI (Digital Object Identifier) -
Publisher Name - IJCRT | www.ijcrt.org | ISSN : 2320-2882
E-ISSN Number - 2320-2882
Cite this article
Shakeel Ahmad, Devesh Kumar, "AERODYNAMIC STUDY OF FLOW THROUGH CONVERGENT-DIVERGENT NOZZLE AND STUDY OF VARIOUS PARAMETERS BY USING ANSYS15.0", International Journal of Creative Research Thoughts (IJCRT), ISSN:2320-2882, Volume.9, Issue 9, pp.a589-a597, September 2021, Available at :http://www.ijcrt.org/papers/IJCRT2109072.pdf
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ISSN: 2320-2882 Impact Factor: 7.97 and ISSN APPROVED Journal Starting Year (ESTD) : 2013
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ISSN: 2320-2882 Impact Factor: 7.97 and ISSN APPROVED Journal Starting Year (ESTD) : 2013
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