43
®
Table 1: Flow calculation table
Profile
Position
Excess Air
Ex. Air + 100
y = x + 100
c = a + 100
d =b + 100
Ratio
Airflow
Fuelflow
High fire
= A
x
y
1 = A
a
1
b
1
c
1
d
1
e
1
+c
1
/d
1
f
1
= e
1
(99.9)
g
1
= f
1
(y/c
1
)
2 = A
a
2
b
2
c
2
d
2
e
2
+c
2
/d
2
f
2
= e
2
(f
1
)
g
2
= f
2
(y/c
2
)
3 = A
a
3
b
3
c
3
d
3
e
3
+c
3
/d
3
f
3
= e
3
(f
2
)
g
3
= f
3
(y/c
2
3)
4 = A
a
4
b
4
c
4
d
4
e
4
+c
4
/d
4
f
4
= e
4
(f
3
)
g
4
= f
4
(y/c
4
)
5 = A
a
5
b
5
c
5
d
5
e
5
+c
5
/d
5
f
5
= e
5
(f
4
)
g
5
= f
5
(y/c
5
)
6 = A
a
6
b
6
c
6
d
6
e
6
+c
6
/d
6
f
6
= e
6
(f
5
)
g
6
= f
6
(y/c
6
)
7 = A
a
7
b
7
c
7
d
7
e
7
+c
7
/d
7
f
7
= e
7
(f
6
)
g
7
= f
7
(y/c
7
)
8 = A
a
8
b
8
c
8
d
8
e
8
+c
8
/d
8
f
8
= e
8
(f
7
)
g
8
= f
8
(y/c
8
)
9 = A
a
9
b
9
c
9
d
9
e
9
+c
9
/d
9
f
9
= e
9
(f
8
)
g
9
= f
9
(y/c
9
)
10 = A
a
10
b
10
c
10
d
10
e
10
+c
10
/d
10
f
10
= e
10
(f
9
)
g
10
= f
10
(y/c
10
)
11 = A
a
11
b
11
c
11
d
11
e
11
+c
11
/d
11
f
11
= e
11
(f
10
) g
11
= f
11
(y/c
11
)
12 = A
a
12
b
12
c
12
d
12
e
12
+c
12
/d
12
f
12
= e
12
(f
11
) g
12
= f
12
(y/c
12
)
13 = A
a
13
b
13
c
13
d
13
e
13
+c
13
/d
13
f
13
= e
13
(f
12
) g
13
= f
13
(y/c
13
)
14 = A
a
14
b
14
c
14
d
14
e
14
+c
14
/d
14
f
14
= e
14
(f
13
)
g
14
= f
14
(y/c
14
)
15 = A
a
15
b
15
c
15
d
15
e
15
+c
15
/d
15
f
15
= e
15
(f
14
) g
15
= f
15
(y/c
15
)
16 = A
a
16
b
16
c
16
d
16
e
16
+c
16
/d
16
f
16
= e
16
(f
15
)
g
16
= f
16
(y/c
16
)
17 = A
a
17
b
17
c
17
d
17
e
17
+c
17
/d
17
f
17
= e
17
(f
16
) g
17
= f
17
(y/c
17
)
18 = A
a
18
b
18
c
18
d
18
e
18
+c
18
/d
18
f
18
= e
18
(f
17
) g
18
= f
18
(y/c
18
)
19 = A
a
19
b
19
c
19
d
19
e
19
+c
19
/d
19
f
19
= e
19
(f
18
) g
19
= f
19
(y/c
19
)
20 = A
a
20
b
20
c
20
d
20
e
20
+c
20
/d
20
f
20
= e
20
(f
19
) g
20
= f
20
(y/c
20
)