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>