Table 1: Contour conditions.

Combustor inlet 𝑇 1 = 124.0°C 𝑇 2 = 101.0°C 𝑇 3 = 80.0°C 𝑣 = 2 . 2 3 3  m s−1
Primary air inlet 𝑇 = 19.3°C 𝑣 = 2 . 1 2 7  m s−1
Secondary air inlet 𝑇 = 19.3°C 𝑣 = 2 . 1 2 7  m s−1
WallsAdiabaticNo sliding
Outlet 𝜕 𝑇 / 𝜕 𝑢 = 0 𝑣 = 6 . 5 6  m s−1 𝑃 = 0  Pa