Effects of Turbulent Reynolds Number on the Performance of Algebraic Flame Surface Density Models for Large Eddy Simulation in the Thin Reaction Zones Regime: A Direct Numerical Simulation Analysis

Figure 1

Contours of 𝑐 in the 𝑥₁-𝑥₂ midplane at time 𝑡=𝛿_th/𝑆_𝐿 for: (a–e) cases A–E.

(a)

(b)

(c)

(d)

(e)