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This paper presents the supersonic combustion of hydrogen fuel using cavity-based fuel injector with two-dimensional turbulent non-premixed combustion model. The present model is based on the standard k-epsilon (two equations) with standard wall functions which is P1 radiation model and a PDF (Probability Density Function) approach is created. The hydrogen fuel is injected just upstream of the cavity. The Contour of Mass fraction of OH indicates a little amount of OH around 0.001454 after combustion. A cavity flame holder is provided which injects hydrogen fuel in a supersonic hot air stream that facilitates enhanced mixing and combustion efficiency.
K.M.Pandey, A.P.Singh. 2012. "Computational Analysis of Combustion Chamber Using Cavity-based fuel Injector with Non-Premixed Combustion Model". Global Journal of Research in Engineering - A : Mechanical & Mechanics GJRE-A Volume 12 (GJRE Volume 12 Issue A3).
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
v1.2
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Total Score: 108
Country: India
Subject: Global Journal of Research in Engineering
Authors: Dr. Jyoti Prakash Kalita, K.M.Pandey, A.P.Singh (PhD/Dr. count: 1)
View Count (all-time): 388
Total Views (Real + Logic): 1130
Total Downloads (simulated): 61
Publish Date: 2012 01, Sun
Monthly Totals (Real + Logic):
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