An example of a generic decompression model is shown below. A
schematic figure of the model is shown along with a typical maximum pressure
output file for a single hole location an a plot of compartment pressure
decay. The decompression model schematic is a greatly simplified
representation of the decompression model primarily indicating connectivity
between volumes.
#AIRLINE
DECOMPRESSION VERIFICATION MODEL - Primary Flight Deck
#COMPARTMENT
MAXIMUM DIFFERENTIAL PRESSURES (PSI)
#HOLE
LOCATED IN COMPARTMENT: 1
#Palt
= 22600.0 FT
#Pamb
= 6.049 PSIA
Comp_a
-> Comp_b +/- Max dp (psid) Time (sec)
----------------
------------------ --------------------
1
- 2 0.00 /
-5.50 0.000 / 0.029
1
- 8 0.00 /
-5.36 0.000 / 0.027
1
- 9 0.00 /
-5.41 0.000 / 0.028
2
- 3 0.00 /
-0.12 0.000 / 0.060
2
- 11 0.02 /
-0.14 0.000 / 0.057
2
- 12 1.18 /
-0.08 2.284 / 0.025
7
- 11 0.02 /
-1.25 0.011 / 2.233
7
- 12 0.05 /
0.00 0.046 / 0.000
8
- 6 0.00 /
-0.4 0.001 / 0.049
9
- 6 0.00 /
-0.36 0.001 / 0.049
5
- 9 0.00 /
-1.15 0.001 / 0.048
5
- 8 0.00 /
-1.07 0.001 / 0.048
15
- 6 0.03 /
0.00 0.045 / 0.000
3
- 11 0.02 /
-0.02 0.381 / 0.004
7
- 15 0.01 /
0.00 0.047 / 0.001
8
- 12 0.00 /
-0.43 0.001 / 0.049
9
- 11 0.02 /
-1.33 0.001 / 1.995
4
- 5 1.21 /
0.00 0.044 / 0.001
5
- 13 0.00 /
-0.77 0.001 / 0.047
13
- 14 0.00 /
-0.32 0.001 / 0.049
9
- 14 0.08 /
0.00 1.142 / 0.001
6
- 11 0.02 /
-1.26 0.005 / 2.215
6
- 13 0.73 /
0.00 0.049 / 0.000
6
- 14 0.41 /
0.00 0.049 / 0.001
6
- 12 0.01 /
0.00 0.050 / 0.001
5
- 6 0.00 /
-1.50 0.001 / 0.048
5
- 7 0.00 /
-1.54 0.001 / 0.048
1
- 6 0.00 /
-5.58 0.000 / 0.029
1
- 5 0.00 /
-4.95 0.000 / 0.024
