Stuart Buchanan
Modifications by Kwanza
22.03.2008
0.2
Models an Avro Vulcan B2.
Manufacturer: Avro Hawker Siddeley Aviation
Length: 99 ft 11 in (30.45 m) 105 ft 6 in (32.16 m)
Length of Nose Probe: 5 ft 7 in (1.71 m)
Wing Span: 111 ft 0 in (33.83 m)
Wing Area: 3,964 sq ft (368.3 m2)
Wing Aspect Ratio: 3.1082
Wing Root Chord: 68.6764 ft
Tip chord: 2.7471 ft
Standard mean chord: 35.7117 ft
Wing Dihedral Angle: -0.85 degrees
Wing setting (incidence) angle: 0
Sweepback of the leading edge: 52.43 degrees
Sweepback of the quarter chord: 45.0845 degrees
Height: 27.17 ft (8.28 m)
Empty Weight: 83,573 lbs / 37,908 kg; 106,000 lbs (48,081 kg) equipped and crewed
Max takeoff weight: 250,000 lbs / 113,398 kg
Crew: 5 (pilot, co-pilot, AEO, Navigator Radar, Navigator Plotter)
Fuel capacity: ,260 imp gal (11,120 US gal; 42,100 l) / 74,240 lb (33,602 kg)
========================
Engines: 4 x Bristol-Siddeley Olympus 301 engines of 20,000 lbf (89 kN) each.
Service Ceiling: 45,000 to 56,000 ft (14,000 to 17,000 m)
Maximum Speed: Mach 0.92 with 301 engines; 561 kts (644 mph, 1,039 km/h)
Cruising Speed: Mach 0.86 at 45,000 feet (14,000 m); 493 kts (567 mph, 913 km/h)
Range: 4,603 mi (4,000 nmi / 7,408 km)
========================
Rotation speed: 150 knots
Refusal speed:
Takeoff speed:
Undercarriage lowering: 270 knots
========================
Landing
weight:
Final speed: 160 knots
Landing speed: 135 knots
=========================
3964.00
111.00
0.00
45.85
991.00
44.96
792.80
44.96
659.45
0.00
0.00
83.93
-30.00
70.00
0.0
0.0
0.0
499661.75
935390.88
1526959.88
0
0
0
83573
651.23
0.00
-29.98
5-man crew at 200 lbs each
1000
8.00
0.00
1.00
Minimum weight of equipment
21177
13.00
0.00
1.00
Payload of bombs and missiles
0
15.00
0.00
-0.45
380.811
0.00
-114.263
0.80
0.50
0.02
75000.00
37500.00
5.00
NONE
1
721.303
-189.224
-114.263
0.80
0.50
0.02
250000.00
125000.00
0
LEFT
1
746.646
-189.224
-114.263
0.80
0.50
0.02
250000.00
125000.00
0
LEFT
1
721.303
189.224
-114.263
0.80
0.50
0.02
250000.00
125000.00
0
RIGHT
1
746.646
189.224
-114.263
0.80
0.50
0.02
250000.00
125000.00
0
RIGHT
1
1054.00
-660.50
-19.70
1
1
250000.00
250000.00
1054.00
660.50
-19.70
1
1
250000.00
250000.00
1162.0
0.0
-29.0
0.80
0.50
250000.00
125000.00
1164.0
0.0
211.0
0.80
0.50
250000.00
125000.00
0.0
0.0
0.0
0.80
0.50
250000.00
125000.00
1064.00
-92.00
-58.00
0.00
0.00
0.00
0
3
4
6
1064.00
-92.00
-58.00
0.00
0.00
0.00
1064.00
-140.00
-58.00
0.00
0.00
0.00
1
2
5
1064.00
-140.00
-58.00
0.00
0.00
0.00
1064.00
92.00
-58.00
0.00
0.00
0.00
7
10
11
13
1064.00
92.00
-58.00
0.00
0.00
0.00
1064.00
140.00
-58.00
0.00
0.00
0.00
8
9
12
1064.00
140.00
-58.00
0.00
0.00
0.00
1000
0
0
0.00
0.00
0.00
1
8
100
0
0
0.00
0.00
0.00
259.38
-50.00
-29.97
5040.0
5000.0
1
JP-1
300.38
-50.00
-29.97
7600.0
7600.0
1
JP-1
659.38
-160.00
-29.97
5040.0
3402.0
2
JP-1
720.38
-160.00
-29.97
5040.0
4032.0
3
JP-1
720.38
-200.00
-29.97
4104.0
2873.0
4
JP-1
759.38
-160.00
-29.97
5896.0
3715.0
2
JP-1
759.38
-200.00
-29.97
4400.0
2772.0
5
JP-1
259.38
50.00
-29.97
5040.0
5000.0
1
JP-1
300.38
50.00
-29.97
7600.0
7600.0
1
JP-1
659.38
160.00
-29.97
5040.0
3402.0
2
JP-1
720.38
160.00
-29.97
5040.0
4032.0
2
JP-1
720.38
200.00
-29.97
4104.0
2873.0
3
JP-1
759.38
160.00
-29.97
5896.0
3715.0
3
JP-1
759.38
200.00
-29.97
4400.0
2772.0
4
JP-1
-45
90
10.0
60.0
Lift due to alpha
aero/qbarUW-psf
metrics/Sw-sqft
aero/alpha-rad
-1.57 0.0000
-1.22 -0.5427
-1.05 -0.7312
-0.88 -0.844
-0.52 -0.600
-0.10 0.000
0.00 0.150
0.17 0.700
0.35 1.200
0.44 1.250
0.52 1.275
0.70 1.150
0.87 0.800
1.05 0.600
1.22 0.450
1.40 0.200
1.57 0.000
Lift due to pitch rate
aero/qbarUW-psf
metrics/Sw-sqft
velocities/q-aero-rad_sec
aero/ci2vel
2.0497
Delta Lift due to speedbrake
aero/qbarUW-psf
metrics/Sw-sqft
fcs/speedbrake-pos-norm
-0.08
Lift due to Elevator Deflection
aero/qbarUW-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.4375
Minimum drag
aero/qbar-psf
metrics/Sw-sqft
0.0068
Drag due to alpha
aero/qbar-psf
metrics/Sw-sqft
aero/alpha-rad
-1.57 1.4081
-0.15 0.0295
0.00 0.0000
0.15 0.0295
1.57 1.4081
Induced drag
aero/qbar-psf
metrics/Sw-sqft
aero/cl-squared
0.042
Drag due to mach
aero/qbar-psf
metrics/Sw-sqft
velocities/mach
0.00 0.0000
0.79 0.0000
1.10 0.0230
1.80 0.0150
Drag due to sideslip
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-1.57 1.2300
-0.26 0.0500
0.00 0.0000
0.26 0.0500
1.57 1.2300
Drag due to Elevator Deflection
aero/qbar-psf
metrics/Sw-sqft
fcs/elevator-pos-rad
0.0400
Drag due to gear
aero/qbar-psf
metrics/Sw-sqft
gear/gear-pos-norm
0.0150
Drag due to speedbrakes
aero/qbar-psf
metrics/Sw-sqft
fcs/speedbrake-pos-norm
0.1200
Drag due to braking chute
aero/qbar-psf
metrics/Sw-sqft
/controls/flight/chute-pos-norm
0.3
Side force due to beta
aero/qbar-psf
metrics/Sw-sqft
aero/beta-rad
-0.9543
Side force due to roll rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/p-aero-rad_sec
aero/Re
66579892 0.1938
73237888 0.0194
99869840 0.0086
186423680 0.0025
Side force due to yaw rate
aero/qbar-psf
metrics/Sw-sqft
aero/bi2vel
velocities/r-aero-rad_sec
0.7731
Side force due to rudder
aero/qbar-psf
metrics/Sw-sqft
fcs/rudder-pos-rad
0.2813
Pitch moment due to alpha
aero/qbarUW-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/alpha-rad
-0.1380
Pitch moment due to elevator
aero/qbarUW-psf
metrics/Sw-sqft
metrics/cbarw-ft
fcs/elevator-pos-rad
velocities/mach
0.0 -1.300
2.0 -0.325
Pitch moment due to pitch rate
aero/qbarUW-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
velocities/q-aero-rad_sec
-21
Pitch moment due to alpha rate
aero/qbarUW-psf
metrics/Sw-sqft
metrics/cbarw-ft
aero/ci2vel
aero/alphadot-rad_sec
-1.5738
Roll moment due to beta
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
gear/gear-no-wow
-0.1
Roll moment due to roll rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-aero-rad_sec
-0.2768
Roll moment due to yaw rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
0.15
Roll moment due to aileron
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
velocities/mach
0.0 0.1000
2.0 0.0250
Roll moment due to rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
0.0100
Yaw moment due to beta
aero/qbarUV-psf
metrics/Sw-sqft
metrics/bw-ft
aero/beta-rad
0.1858
Yaw moment due to roll rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/p-rad_sec
aero/Re
66579892 -0.0785
73237888 -0.0079
99869840 -0.0035
186423680 -0.0010
Yaw moment due to yaw rate
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
aero/bi2vel
velocities/r-aero-rad_sec
-0.1535
Yaw moment due to rudder
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/rudder-pos-rad
-0.1139
Adverse yaw
aero/qbar-psf
metrics/Sw-sqft
metrics/bw-ft
fcs/left-aileron-pos-rad
0.0000
aero/qbar-psf
/controls/flight/chute-pos-norm
115
97.7492
0
0
-1
0
0