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Proc. ASME. IMECE2021, Volume 11: Heat Transfer and Thermal Engineering, V011T11A021, November 1–5, 2021
Paper No: IMECE2021-69458
... with turbulent Schmidt number 0.20 can be considered for the reasonable estimation of the supersonic mixing flow field. Keywords: Scramjet, Turbulence, Schmidt Number, Flow Separation, Bow Shock 1. INTRODUCTION Ensuring proper mixing of fuel with the incoming supersonic air stream is one of the most challenging...
Proc. ASME. IMECE2013, Volume 1: Advances in Aerodynamics, V001T01A046, November 15–21, 2013
Paper No: IMECE2013-66036
... In the arena of design of combustion chamber of scramjet engine lots of development are still going on. A properly designed combustor shall promote sufficient mixing of the fuel and air so that the desired chemical reaction and thus heat release can occur within the limited residence time...
Proc. ASME. IMECE2011, Volume 4: Energy Systems Analysis, Thermodynamics and Sustainability; Combustion Science and Engineering; Nanoengineering for Energy, Parts A and B, 1521-1529, November 11–17, 2011
Paper No: IMECE2011-62310
... 02 08 2012 The simulation of a supersonic reactive flow is an important tool for the investigation and development of Scramjet engines. Numerical investigations have become less expensive than experiments. In this research work mixing and combustion for different type of strut injector...
Proc. ASME. IMECE2004, Energy Conversion and Resources: Fuels and Combustion Technologies, Energy, Nuclear Engineering, 131-134, November 13–19, 2004
Paper No: IMECE2004-61326
... 28 03 2008 The purpose of this research is to accurately simulate combustion in a scramjet engine using a CFD (Computational Fluid Dynamics) software package called Fluent and to validate the results with existing experimental data from NASA Langley Research Center. The use...