[Jsbsim-cvslogs] CVS: JSBSim/engine GE-CF6-80C2-B1F.xml,1.1,1.2

[Jon S. B. <jb...@us...>]

Update of /cvsroot/jsbsim/JSBSim/engine
In directory sc8-pr-cvs1.sourceforge.net:/tmp/cvs-serv9733/engine

Modified Files:
	GE-CF6-80C2-B1F.xml 
Log Message:
Changes to the Propagate mode - removed VRP items to FGAuxiliary, etc.; removed FGTurbine

Index: GE-CF6-80C2-B1F.xml
===================================================================
RCS file: /cvsroot/jsbsim/JSBSim/engine/GE-CF6-80C2-B1F.xml,v
retrieving revision 1.1
retrieving revision 1.2
diff -C2 -r1.1 -r1.2
*** GE-CF6-80C2-B1F.xml	18 Mar 2004 12:50:41 -0000	1.1
--- GE-CF6-80C2-B1F.xml	24 Apr 2004 17:13:00 -0000	1.2
***************
*** 1,94 ****
! <?xml version="1.0"?>

! <!--

!   File:     GE-CF6-80C2-B1F.xml

!   Author:   Jon Berndt, based on output from

!             Aero-Matic v 0.7, by David Culp

! 

!   Inputs:

!     name:           GE-CF6-80C2-B1F

!     type:           turbine

!     thrust:         58000.0 lb

!     augmented?      no

!     injected?       yes

! 

!   Additional Information:

! 

!   [Source: http://www.bh.com/companions/034074152X/appendices/data-b/table-3/default.htm]

! 

!     Number of shafts: 2

!     Compressor: 1 + 4LP

!                 14HP

!     Turbine:    2HP, 5LP

!     Cost: $6.10 million

! 

!     Length: 14.00 ft.

!     Fan diameter: 8.84 ft.

!     Weight: 9,500 lbs.

! 

!     Flat rating: 32 degrees C

!     Pressure ratio (TO): 29.90

!     Mass flow (lb/sec, TO): 1,765 (lb/sec)

!     TSFC (TO): 0.32

! -->

! 

! <FG_SIMTURBINE NAME="GE-CF6-80C2-B1F">

!   MILTHRUST 58000.0

!   MAXTHRUST 58000.0

!   BYPASSRATIO    5.15

!   TSFC           0.564

!   ATSFC          0.0

!   IDLEN1        30.0

!   IDLEN2        60.0

!   MAXN1        100.0

!   MAXN2        100.0

!   AUGMENTED      0

!   AUGMETHOD      1

!   INJECTED       1

! 

! <TABLE NAME="IdleThrust" TYPE="TABLE">

!   Idle_power_thrust_factor

!   6

!   7

!   velocities/mach-norm

!   position/h-sl-ft

!   none

!        -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     0.0     0.0276  0.0718  0.1073

!   0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900

!   1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800

! </TABLE>

! 

! <TABLE NAME="MilThrust" TYPE="TABLE">

!   Military_power_thrust_factor

!   8

!   7

!   velocities/mach-norm

!   position/h-sl-ft

!   none

!         -10000       0   10000   20000   30000   40000   50000

!   0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490

!   0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430

!   0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450

!   0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540

!   0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700

!   1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950

!   1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250

!   1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630

! </TABLE>

! 

! <TABLE NAME="WaterFactor" TYPE="TABLE">

!   Water_injection_factor

!   2

!   2

!   velocities/mach-norm

!   position/h-sl-ft

!   none

!               0  50000

!   0.0    1.2000  1.2000

!   1.0    1.2000  1.2000

! </TABLE>

! 

! </FG_SIMTURBINE>

--- 1,94 ----
! <?xml version="1.0"?>
! <!--
!   File:     GE-CF6-80C2-B1F.xml
!   Author:   Jon Berndt, based on output from
!             Aero-Matic v 0.7, by David Culp
! 
!   Inputs:
!     name:           GE-CF6-80C2-B1F
!     type:           turbine
!     thrust:         58000.0 lb
!     augmented?      no
!     injected?       yes
! 
!   Additional Information:
! 
!   [Source: http://www.bh.com/companions/034074152X/appendices/data-b/table-3/default.htm]
! 
!     Number of shafts: 2
!     Compressor: 1 + 4LP
!                 14HP
!     Turbine:    2HP, 5LP
!     Cost: $6.10 million
! 
!     Length: 14.00 ft.
!     Fan diameter: 8.84 ft.
!     Weight: 9,500 lbs.
! 
!     Flat rating: 32 degrees C
!     Pressure ratio (TO): 29.90
!     Mass flow (lb/sec, TO): 1,765 (lb/sec)
!     TSFC (TO): 0.32
! -->
! 
! <FG_SIMTURBINE NAME="GE-CF6-80C2-B1F">
!   MILTHRUST 58000.0
!   MAXTHRUST 58000.0
!   BYPASSRATIO    5.15
!   TSFC           0.564
!   ATSFC          0.0
!   IDLEN1        30.0
!   IDLEN2        60.0
!   MAXN1        100.0
!   MAXN2        100.0
!   AUGMENTED      0
!   AUGMETHOD      1
!   INJECTED       1
! 
! <TABLE NAME="IdleThrust" TYPE="TABLE">
!   Idle_power_thrust_factor
!   6
!   7
!   velocities/mach-norm
!   position/h-sl-ft
!   none
!        -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     0.0     0.0276  0.0718  0.1073
!   0.8  0.0     0.0     0.0     0.0     0.0474  0.0868  0.0900
!   1.0  0.0     0.0     0.0     0.0     0.0     0.0552  0.0800
! </TABLE>
! 
! <TABLE NAME="MilThrust" TYPE="TABLE">
!   Military_power_thrust_factor
!   8
!   7
!   velocities/mach-norm
!   position/h-sl-ft
!   none
!         -10000       0   10000   20000   30000   40000   50000
!   0.0   1.2600  1.0000  0.7400  0.5340  0.3720  0.2410  0.1490
!   0.2   1.1710  0.9340  0.6970  0.5060  0.3550  0.2310  0.1430
!   0.4   1.1500  0.9210  0.6920  0.5060  0.3570  0.2330  0.1450
!   0.6   1.1810  0.9510  0.7210  0.5320  0.3780  0.2480  0.1540
!   0.8   1.2580  1.0200  0.7820  0.5820  0.4170  0.2750  0.1700
!   1.0   1.3690  1.1200  0.8710  0.6510  0.4750  0.3150  0.1950
!   1.2   1.4850  1.2300  0.9750  0.7440  0.5450  0.3640  0.2250
!   1.4   1.5941  1.3400  1.0860  0.8450  0.6280  0.4240  0.2630
! </TABLE>
! 
! <TABLE NAME="WaterFactor" TYPE="TABLE">
!   Water_injection_factor
!   2
!   2
!   velocities/mach-norm
!   position/h-sl-ft
!   none
!               0  50000
!   0.0    1.2000  1.2000
!   1.0    1.2000  1.2000
! </TABLE>
! 
! </FG_SIMTURBINE>