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
Walls
Adiabatic
No sliding
Outlet
𝜕
𝑇
/
𝜕
→
𝑢
=
0
𝑣
=
6
.
5
6
m s
−1
𝑃
=
0
Pa