Fokker50 > Flight Dynamic

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Our products feature a 'Art of Machine' philosophy, so we are not only specially great on precise Modeling, but also strong in Flight Dynamic. We try our best to input the real data on flight dynamic files, then being the intensive flight dynamic test. 



The real data are already inputed as follows:

Weight_and_balance:
max_gross_weight = 45900
empty_weight = 27602

Station playload for 50 passengers:
Pilot = 170 lbs
Co-Pilot = 170 lbs
A Cabin Crew = 170 lbs
Front Cargo = 1200 lbs
1A + 1B = 340 lbs
2A + 2B + 2C + 2D = 680 lbs
3A + 3B + 3C + 3D = 680 lbs
4A + 4B + 4C + 4D = 680 lbs
5A + 5B + 5C + 5D = 680 lbs
6A + 6B + 6C + 6D = 680 lbs
7A + 7B + 7C + 7D = 680 lbs
8A + 8B + 8C + 8D = 680 lbs
9A + 9B + 9C + 9D = 680 lbs
10A + 10B + 10C + 10D = 680 lbs
11A + 11B + 11C + 11D = 680 lbs
12A + 12B + 12C + 12D = 680 lbs
13A + 13B + 13C + 13D = 680 lbs
A Cabin Crew = 170 lbs
Rear Cargo = 1600 lbs

Fuel playload for 2 main tanks:
Max. fuel load = 4,123 kg / 9,090 lb

Turboprop_engine & Propeller:
rated_N2_rpm = 27700  (NL: low-pressure engine speed)
Maximum torque available = 10750
propeller_diameter = 12
propeller_blades = 6
Engine Max. rpm = 1200

Airplane Geometry:
wing_area = 754 ft/sq.
wing_span = 95.15 ft
wing_root_chord = 11.367 ft
wing_dihedral = 2.5 degree
wing_incidence = 3.5 degree
wing_twist = 0.0 degree
oswald_efficiency_factor = 0.75
wing_winglets_flag = yes
wing_sweep = 3.5 degree
wing_pos_apex_lon = 2.7 ft
wing_pos_apex_vert = -0.56 ft
htail_area = 172.2 ft/sq.
htail_span = 32.0 ft/sq.
htail_pos_lon = -33.79
htail_pos_vert = 1.69
htail_incidence = 12 degree
htail_sweep = 11.5 degree
vtail_area = 153.0 ft/sq.
revtail_span = 15.18  ft/sq.
vtail_sweep = 23.0  ft/sq.
vtail_pos_lon = -32.02000
vtail_pos_vert = 0.67000
elevator_area = 50.72 ft/sq.
aileron_area = 25.8 ft/sq.
rudder_area = 41.65 ft/sq.
elevator_up_limit = 25.0 degree
elevator_down_limit = 22.0 degree
aileron_up_limit = 33.0 degree
aileron_down_limit = 22.0 degree
rudder_limit = 20.0 degree
elevator_trim_limit = 27.0 degree



Last Updated on Wednesday, 19 June 2013 03:59

 

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Fokker 50/60 : Vref. is the landing threshold speed during final approach at a height of 50 feet above the runway. Recommended final approach speed is Vref. + 10 knots.

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