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Advances in Aerodynamics

Table 3 Operation conditions for the θ-parameter sensitivity study

From: Numerical study on the combustion process in a gas turbine combustor with different reference velocities

No

P [atm]

Tinlet [K]

Uref [m/s]

θ-parameter

1

0.5

300

25

6.65 × 106

2

0.5

300

18

9.23 × 106

3

1

300

25

1.12 × 107

4

0.5

400

25

1.24 × 107

5

1

300

18

1.55 × 107

6

1

400

25

2.08 × 107

7

0.5

538

25

2.63 × 107

8

1

538

25

4.43 × 107

9

0.5

538

10

6.59 × 107

10

6.5

400

25

8.47 × 107

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