From 976c285ad7d11718f07352e3d57d155e4b325e58 Mon Sep 17 00:00:00 2001
From: ehofman <ehofman>
Date: Sat, 17 Jan 2004 10:35:22 +0000
Subject: [PATCH] Match the changes of the 737 and OV10

---
 Engine/CFM56_sim.xml |  5 +++--
 Engine/T76_sim.xml   | 16 ++++++----------
 2 files changed, 9 insertions(+), 12 deletions(-)

diff --git a/Engine/CFM56_sim.xml b/Engine/CFM56_sim.xml
index bfa949ff1..d2eb047d0 100644
--- a/Engine/CFM56_sim.xml
+++ b/Engine/CFM56_sim.xml
@@ -1,7 +1,8 @@
 <?xml version="1.0"?>
 
 <!-- CFM56 turbofan engine model
-     Version 1.0, 14 Mar 2003, David Culp, davidculp2@attbi.com
+     Version 1.0, 14 Mar 2003, David Culp, davidculp2@comcast.net
+     Updated 20 Oct 2003, DPC, new MAXTHRUST item
 -->
 
 <FG_SIMTURBINE NAME="CFM56">
@@ -45,7 +46,7 @@
     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
+    0.0    0.0483  0.0528  0.0694  0.0899  0.1183  0.1467
     0.2    0.0501  0.0335  0.0544  0.0797  0.1049  0.1341
     0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
     0.6   -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073
diff --git a/Engine/T76_sim.xml b/Engine/T76_sim.xml
index 659831db2..8d423f2f5 100644
--- a/Engine/T76_sim.xml
+++ b/Engine/T76_sim.xml
@@ -40,18 +40,14 @@
 
   <TABLE NAME="IdleThrust" TYPE="TABLE">
     Idle_power_thrust_factor
-    6
-    6
+    2
+    2
     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  0.1341
-    0.4    0.0047  0.0020  0.0272  0.0595  0.0891  0.1203
-    0.6   -0.0804 -0.0560 -0.0237  0.0276  0.0718  0.1073
-    0.8   -0.2129 -0.1498 -0.1025 -0.0195  0.0473  0.0868
-    1.0   -0.2839 -0.1104 -0.0469 -0.0270 -0.0158  0.0552
+                0  40000
+    0.0    0.0000  0.0000
+    1.0    0.0000  0.0000
   </TABLE>
 
  <TABLE NAME="MilThrust" TYPE="TABLE">
@@ -65,7 +61,7 @@
   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
+  0.6    0.3210  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
  </TABLE>