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integration of cfd and low-order models for combustion ... - IWR

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0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

1800<br />

1600<br />

1400<br />

1200<br />

CFD result<br />

with J1 ′<br />

without J1 ′<br />

2.5<br />

2<br />

1000<br />

| T ′ |<br />

800<br />

600<br />

400<br />

| F ′ |<br />

1.5<br />

1<br />

200<br />

0.5<br />

0<br />

0<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

250<br />

200<br />

150<br />

CFD result<br />

with J1 ′<br />

without J1 ′<br />

0<br />

100<br />

−50<br />

angle [ T ′ ] deg.<br />

50<br />

0<br />

−50<br />

−100<br />

angle [ F ′ ] deg.<br />

−100<br />

−150<br />

−150<br />

−200<br />

−200<br />

−250<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

Figure 14. Magnitude <strong>and</strong> phase <strong>of</strong> the transfer function between<br />

the temperature <strong>and</strong> air f<strong>low</strong> rate through the atomizer at a<br />

frequency 50 Hz, where the solid lines indicate the result from the<br />

CFD calculation. The dash lines <strong>and</strong> dotted-dash lines indicate the<br />

results from one-dimensional analysis with <strong>and</strong> without J?1 ,<br />

respectively.<br />

Figure 16.<br />

−250<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

Magnitude <strong>and</strong> phase <strong>of</strong> the transfer function between<br />

shape factor F <strong>and</strong> air f<strong>low</strong> rate through the atomizer at a frequency<br />

50 Hz.<br />

450<br />

120<br />

400<br />

CFD result<br />

100<br />

CFD result<br />

with J1 ′<br />

without J1 ′<br />

350<br />

300<br />

with F ′ J2 ′<br />

without F ′ J2 ′<br />

80<br />

250<br />

| T ′ |<br />

200<br />

| u ′ |<br />

60<br />

150<br />

40<br />

100<br />

50<br />

20<br />

0<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

0<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

200<br />

150<br />

150<br />

CFD result<br />

100<br />

CFD result<br />

with J1 ′<br />

100<br />

with F ′ J2 ′<br />

without F ′ J2 ′<br />

without J1 ′<br />

50<br />

angle [ u ′ ] deg.<br />

50<br />

0<br />

−50<br />

−100<br />

−150<br />

angle [ T ′ ] deg.<br />

0<br />

−50<br />

−100<br />

−150<br />

−200<br />

−250<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

Figure 15.<br />

−200<br />

0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22<br />

Magnitude <strong>and</strong> phase <strong>of</strong> the transfer function between<br />

the velocity <strong>and</strong> air f<strong>low</strong> rate through the atomizer at a frequency<br />

50 Hz, where the solid lines indicate the result from the CFD<br />

calculation. The dash lines <strong>and</strong> dotted-dash lines indicate the<br />

results from one-dimensional analysis with <strong>and</strong> without J?1 ,<br />

respectively.<br />

Figure 17. Magnitude <strong>and</strong> phase <strong>of</strong> the transfer function between<br />

the temperature <strong>and</strong> air f<strong>low</strong> rate through the atomizer at a<br />

frequency 50 Hz, where the solid lines indicate the result from the<br />

CFD calculation. The dash lines <strong>and</strong> dotted-dash lines indicate the<br />

results from one-dimensional analysis with <strong>and</strong> F@ without <strong>and</strong> J@2 ,<br />

respectively.

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