Large eddy simulations of the HIFiRE scramjet using a compressible flamelet/progress variable approach

Amirreza Saghafian; Lee Shunn; David Philips; Frank Ham

doi:10.1016/j.proci.2014.10.004

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Large eddy simulations of the HIFiRE scramjet using a compressible flamelet/progress variable approach

Amirreza Saghafian Lee Shunn David Philips Frank Ham

Year: 2014 Journal: Proceedings of the Combustion Institute Vol: 35 (2)Pages: 2163-2172 Publisher: Elsevier BV

DOI: 10.1016/j.proci.2014.10.004

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Keywords:

Scramjet Mach number Compressibility Supersonic speed Mechanics Large eddy simulation Combustor Combustion Compressible flow Aerospace engineering Physics Materials science Thermodynamics Turbulence Engineering Chemistry

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Combustion and flame dynamics

Physical Sciences → Engineering → Computational Mechanics

Computational Fluid Dynamics and Aerodynamics

Physical Sciences → Engineering → Computational Mechanics

Rocket and propulsion systems research

Physical Sciences → Engineering → Aerospace Engineering

Large eddy simulations of the HIFiRE scramjet using a compressible flamelet/progress variable approach

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