Please use this identifier to cite or link to this item: http://nopr.niscair.res.in/handle/123456789/30400
Title: Analysis of reacting flows in an aero-engine afterburner using computational fluid dynamics
Authors: Unaune, Sunil V
Ganesan, V
Issue Date: Feb-2004
Publisher: NISCAIR-CSIR, India
Abstract: In this paper, reacting flows in an aero-engine afterburner are analyzed using computational fluid dynamics (CFD). A computational procedure is described for calculating the three-dimensional reacting flow fields in a gas turbine afterburner. The computations are based on numerical solution of time-averaged transport equations for mass, momentum, turbulent kinetic energy and dissipation rate using a finite volume formulation. The numerical calculations are performed using SIMPLE(Semi Implicit Method for Pressure Linked Equations). The RNG (Re-normalization Group Theory) k-ɛ model is used for turbulence modeling. Combustion is modeled using PDF (Probability Density Function). The results for air-fuel Ratio of 30 and 46 are obtained and analyzed.
Page(s): 31-37
URI: http://hdl.handle.net/123456789/30400
ISSN: 0975-1017 (Online); 0971-4588 (Print)
Appears in Collections:IJEMS Vol.11(1) [February 2004]

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