Updates to the Fokker-120NG
[fg:toms-fgdata.git] / Aircraft / fokker100 / Engines / SaM146-1S17.xml
1 <?xml version="1.0"?>
2 <!--
3   File:     SaM146-1S17.xml
4   Author:   Aero-Matic v 0.82
5
6   Inputs:
7     name:           SaM146-1S17
8     type:           turbine
9     thrust:         17273.632 lb (76.84 kN)
10     augmented?      no
11     injected?       no
12
13     fan diameter:   48.2 inches (1.22m)
14     dry weight:     1,708 kg (3,770 lb)
15 -->
16
17 <turbine_engine name="SaM146-1S17">
18   <milthrust> 17273.6 </milthrust>
19   <bypassratio>     4.43 </bypassratio>
20   <tsfc>            0.629 </tsfc>
21   <bleed>           0.03</bleed>
22   <idlen1>         30.0 </idlen1>
23   <idlen2>         60.0 </idlen2>
24   <maxn1>         100.0 </maxn1>
25   <maxn2>         100.0 </maxn2>
26   <augmented>         0 </augmented>
27   <injected>          0 </injected>
28
29   <function name="IdleThrust">
30    <table>
31     <independentVar lookup="row">velocities/mach</independentVar>
32     <independentVar lookup="column">atmosphere/density-altitude</independentVar>
33     <tableData>
34          -10000     0     10000   20000   30000   40000   50000   60000
35      0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467  0
36      0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342  0
37      0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203  0
38      0.6  0.0     0.0     0.0     0.0     0.0276  0.0718  0.1073  0
39      0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900  0
40      1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800  0
41     </tableData>
42    </table>
43   </function>
44
45   <function name="MilThrust">
46    <table>
47     <independentVar lookup="row">velocities/mach</independentVar>
48     <independentVar lookup="column">atmosphere/density-altitude</independentVar>
49     <tableData>
50           -10000       0   10000   20000   30000   40000   50000   60000
51      0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490  0
52      0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430  0
53      0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450  0
54      0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540  0
55      0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700  0
56      1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950  0
57      1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250  0
58      1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630  0
59     </tableData>
60    </table>
61   </function>
62
63 </turbine_engine>
64