dlrk wrote:
If you've made an NGX profile, any chance you could post it?
Hi,
I am on FS9 at the moment - so I don't have a NGX profile. Sorry.
But to give you an idea, how to create such a profile out of this tables, I add here my F100 profile. You will find these values in the file mentioned above. The conversation to the FSBuild format can easily done by Excel or some other spreadsheet program.
(1) Entry in the fsb_Aircraft.cfg file:
Code:
[F100 / MK650-15] -- (R. Brantner) ---
WeightUnit=LBS
OperEmptyWeight=57342
PayloadWeight=23356
HoldFuel=:20
TaxiFuel=33/min
ReserveFuel=%6
AlternateFuel=
ExtraFuel=:45
ApproachFuel=0
Imagefile=F100.jpg
Callsign=AUA668
DefaultTOFlaps=0
DefaultLDGFlaps=42
PerformanceData=F100.prf
ToldData=F100.tld
ClimbFuelBias=+0.0
CruiseFuelBias=+0.0
DescentFuelBias=+0.0
MaxTakeoffWeight=97994
MaxLandingWeight=88000
MaxCruise=35000
FSKneeBoardNotesFileName=\navlog.txt
MaxZeroFuelWeight=80997
MaxFuelWeight=17297
MachCruise=70
(2) F100.PRF in the Aircraft folder:
Code:
[F100] ----------------- F100 (Created by R. Brantner) --------------
[UNITS]
FUEL=kgs/min
WEIGHT=KGS
MACHCRUISE=70
[CLIMB]
;ALT TAS ROC FUEL
0 148 1960 83.8
500 149 1920 82.9
1000 150 1910 81.9
1500 156 1970 81.1
2000 157 1960 80.2
3000 180 2210 78.7
4000 215 2500 77.3
6000 272 2630 74.4
8000 280 2490 71.0
10000 289 2350 67.7
12000 332 2120 64.8
14000 342 1950 61.7
16000 353 1790 58.6
18000 363 1620 55.6
20000 375 1440 52.7
22000 386 1270 49.9
24000 398 1100 47.2
26000 411 930 44.6
28000 416 1080 42.0
29000 414 1020 40.7
31000 411 920 38.2
33000 407 820 35.8
35000 403 700 33.5
[CRUISE]
;ALT TAS FUEL (Mach .70 cruise / (GRWT)
[GRWT] 30 38 43
35000 403 24.7 28.2 30.7
33000 407 26.1 29.3 31.6
31000 411 27.7 30.7 32.8
29000 414 29.6 32.3 34.2
28000 416 30.6 33.1 35.0
26000 411 31.7 34.1 35.9
24000 398 31.8 34.2 36.0
22000 386 32.0 34.3 36.1
20000 375 32.1 34.5 36.2
18000 363 32.2 34.5 36.2
16000 353 32.3 34.6 36.3
14000 306 27.4 30.2 32.3
12000 297 27.4 30.3 32.3
10000 289 27.5 30.3 32.3
8000 280 27.5 30.3 32.3
6000 272 27.5 30.3 32.3
4000 233 23.4 27.0 29.6
3000 230 23.4 27.0 29.6
[DESCENT]
;ALT TAS ROD FUEL
0 139 640 28.4
500 140 660 28.1
1000 146 710 27.8
1500 157 750 13.0
2000 189 1090 10.7
3000 230 1380 10.7
4000 233 1390 10.7
6000 240 1420 10.7
8000 280 1810 10.7
10000 289 1850 10.7
12000 332 2360 10.7
14000 342 2400 10.7
16000 353 2440 10.6
18000 363 2480 10.6
20000 375 2520 10.6
22000 386 2560 10.6
24000 398 2590 10.6
26000 411 2620 10.6
28000 416 3400 10.6
29000 414 3300 10.6
31000 411 1280 17.4
33000 407 1250 16.3
35000 403 1230 16.3
[Altitude]
; --- Altitude Capability (Max at ISA)
;Altiude GrossWt
33000 44000
34000 42000
35000 36000
(3) F100.TLD in the Aircraft folder:
Code:
[F100] --------- F100 -------(Created by Reinhard Brantner)------
TempUnit=Celsius
;
;------------------------------ Takeoff ------------------------------------------
;
; Currently no compensation calculated (all altitudes, all temperatures)
;
; Elevation Temperature C
[Alt-Temp]
-1000 9000 <=50
;
;
; Gross Wt V1-VR-V2
[FLAPS 0]
61729 111-111-119
66139 116-116-123
70548 120-120-128
74957 125-125-132
79366 130-130-135
83776 134-134-139
88185 138-138-143
92594 142-142-149
97003 147-147-150
[FLAPS 8]
61729 107-107-113
66139 112-112-117
70548 116-116-121
74957 120-120-125
79366 123-123-128
83776 127-127-132
88185 131-131-135
92594 135-135-138
97003 139-139-142
[FLAPS 15]
61729 104-104-110
66139 109-109-114
70548 113-113-118
74957 117-117-121
79366 121-121-125
83776 125-125-128
88185 129-129-131
92594 132-132-134
97003 136-136-138
;
;
;------------------------------ Landing ------------------------------------------
;
; Vref speeds
[VREF]
[FLAPS] 0 25 42
61729 129 117 109
66139 134 122 112
70548 138 126 116
74957 142 129 120
79366 146 134 123
83776 150 136 127
88185 154 140 130
92594 158 145 133
97003 162 147 136
For the TLD data I did a simplification and did not implement the temperature correction, as I am using TOPCAT for all these calculations. So I just used the values found for standard environmental conditions.
Reinhard