Modelling n-heptane dilute spray flames in a model supersonic combustor fueled by hydrogen
Abstract
Combustion characteristics of n-heptane dilute sprays in a model supersonic combustor fueled by hydrogen are numerically investigated. The two-phase compressible reactive flows are solved by a Eulerian-Lagrangian framework. Supersonic air enters the combustor at Mach 2.0, whereas hydrogen is injected sonically at the strut base. Monodispersed liquid n-heptane droplets are carried by hydrogen jet at different Spray Equivalence Ratios (SERs),...
Paper Details
Title
Modelling n-heptane dilute spray flames in a model supersonic combustor fueled by hydrogen
Published Date
Mar 1, 2020
Journal
Volume
264
Pages
116809 - 116809
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