From a73075dc127dd6eb9c32543b273c2b31d6461754 Mon Sep 17 00:00:00 2001
From: ehofman <ehofman>
Date: Sat, 10 Apr 2004 13:55:56 +0000
Subject: [PATCH] Updates to match the Fokker 50

---
 Engine/PW125B_sim.xml | 51 +++++++++++++++++++++++--------------------
 1 file changed, 27 insertions(+), 24 deletions(-)

diff --git a/Engine/PW125B_sim.xml b/Engine/PW125B_sim.xml
index 958b22dd4..9661593d9 100644
--- a/Engine/PW125B_sim.xml
+++ b/Engine/PW125B_sim.xml
@@ -1,19 +1,19 @@
 <?xml version="1.0"?>
 <!--
-  File:     PW125B.xml
-  Author:   Aero-Matic v 0.3
+  File:     PW172B.xml
+  Author:   Aero-Matic v 0.7
 
   Inputs:
-    name:           PW125B
+    name:           PW172B
     type:           turboprop
-    power:          2500 hp
+    power:          2750 hp
     augmented?      no
     injected?       no
 -->
-<!-- 2500 horsepower X  2.24 lbs/hp -->
-<FG_SIMTURBINE NAME="PW125B">
-  MILTHRUST   5600.00
-  MAXTHRUST   5600.00
+
+<FG_SIMTURBINE NAME="PW172B">
+  MILTHRUST 6160.00
+  MAXTHRUST 6160.00
   BYPASSRATIO    0.0
   TSFC           0.55
   ATSFC          0.0
@@ -24,34 +24,37 @@
   AUGMENTED      0
   AUGMETHOD      1
   INJECTED       0
+
 <TABLE NAME="IdleThrust" TYPE="TABLE">
   Idle_power_thrust_factor
   6
-  6
+  7
   velocities/mach-norm
   position/h-sl-ft
   none
-              0   10000   20000   30000   40000   50000
-  0.0    0.0836  0.0528  0.0694  0.0899  0.1183  0.1467
-  0.2    0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
-  0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-  0.6    0.0     0.0     0.0     0.0276  0.0718  0.1073
-  0.8    0.0     0.0     0.0     0.0     0.0474  0.0868
-  1.0    0.0     0.0     0.0     0.0     0.0     0.0552
+       -10000       0   10000   20000   30000   40000   50000
+  0.0  0.0430  0.0488  0.0528  0.0694  0.0899  0.1183  0.1467
+  0.2  0.0500  0.0501  0.0335  0.0544  0.0797  0.1049  0.1342
+  0.4  0.0040  0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
+  0.6  0.0     0.0     0.0     0.0276  0.0718  0.0430  0.0
+  0.8  0.0     0.0     0.0     0.0     0.0174  0.0086  0.0
+  1.0  0.0     0.0     0.0     0.0     0.0     0.0     0.0
 </TABLE>
+
 <TABLE NAME="MilThrust" TYPE="TABLE">
   Military_power_thrust_factor
   6
-  6
+  7
   velocities/mach-norm
   position/h-sl-ft
   none
-              0   10000   20000   30000   40000   50000
-  0.0    1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
-  0.2    0.7340  0.6970  0.5060  0.3550  0.2310  0.1430
-  0.4    0.6210  0.5920  0.4060  0.3570  0.2330  0.1450
-  0.6    0.3510  0.2710  0.2020  0.1780  0.1020  0.0640
-  0.8    0.0200  0.0200  0.0200  0.0200  0.0200  0.0200
-  1.0    0.0     0.0     0.0     0.0     0.0     0.0
+       -10000       0   10000   20000   30000   40000   50000
+  0.0  1.1260  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
+  0.2  1.1000  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430
+  0.4  1.0000  0.6410  0.6120  0.4060  0.3570  0.2330  0.1450
+  0.6  0.4430  0.3510  0.2710  0.2020  0.1780  0.1020  0.0640
+  0.8  0.0240  0.0200  0.0160  0.0130  0.0110  0.0100  0.0
+  1.0  0.0     0.0     0.0     0.0     0.0     0.0     0.0
 </TABLE>
+
 </FG_SIMTURBINE>