Dynamics An-24RV (V5.25) for the pack Samdim_An-24RV V2.1 Просмотр ZIP-архива

An-24_dyn_v5.25_oldviz/dynamics/Aircraft.cfg

// Title:	An-24RV dynamics
// Author:	Aless (thanks for the help to Curl, ALZP, UNKL, Agat, Vinni-Puh, Ranger, Jurik ...) 
// Version: v5.25a (for old Samdim visual model)
// Date: june 2012
//full fuel, full equip., pass empty, Baggage 3 = 400kg (100%)
//TOW 19994, MAC=23.62% (with fuel), MAC=24.92 (without fuel)

[fltsim.0]
title=Samdim Design Antonov An-24RV UTAir
sim=Antonov An-24RV
model=
panel=
sound=
texture=utair
atc_airline=utair
atc_flight_number=46501
atc_id=46501
checklists=
ui_manufacturer=Antonov (Samdim Design)
ui_type=An-24RV
ui_variation=UTAir
description=The Legendary Russian Turboprop\nAn-24 is the most used short-range aircraft in the ex-USSR. First flight: september,1 1963. Hundreds are still in service.\n\nFSDS2 model by D.Samborski ([email protected])\nPanel by V.Bocharnikov ([email protected])\nGauges by S.Gritsevsky (c) 2003\nDynamics by A.Terentyev v5.23a (c) 2012\nSounds from Mike Maarse with corrections of S.Teifel (2006)
visual_damage=1
// --- add custom liveries starting from here ---
// [fltsim.2]
// ...
// --- do not modify after this line ---
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[General]
performance=48-52 Passenger\nTwin Turboprop\nRegional Commuter\n\nDevelopment version 
atc_type=Antonov 
atc_model=AN24 
editable=0 

[Propeller]
thrust_scalar=1.0 
propeller_type=0 
propeller_diameter=12.795 
propeller_blades=4 
propeller_moi=300 
beta_max=49.99 
beta_min=8.0 
min_gov_rpm=13900.00 
prop_tc=0.006 
gear_reduction_ratio=12.1285 
fixed_pitch_beta=15 
low_speed_theory_limit=60.0 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=500.000 //1245
beta_feather=93.320 
power_absorbed_cf=1.000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=8.0 
minimum_reverse_beta=0.0 
rotation=-1 -1

[Turboprop_engine]
power_scalar=1.0 
maximum_torque=10614.3602 
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.00 
idle_rpm_friction_scalar=1.0 

[TurbineEngineData]
fuel_flow_gain=0.0045 //0.003
inlet_area=1.000 
rated_N2_rpm=15100 
static_thrust=470 
afterburner_available=0 

[flight_tuning]
cruise_lift_scalar=1.0 
pitch_stability=1.0 
roll_stability=1.000 
yaw_stability=1.000 
parasite_drag_scalar=1.0 
induced_drag_scalar=1.0 
elevator_effectiveness=1.00 
aileron_effectiveness=1.00 
rudder_effectiveness=1.0 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 
hi_alpha_on_roll=1 //multiplier on the effects on roll at high angles of attack
hi_alpha_on_yaw=1 //multiplier on the effects on yaw at high angles of attack
p_factor_on_yaw=1 //multipliers on the effects induced by rotating propellers 
torque_on_roll=1
prop_effect_on_pitch=1
prop_effect_on_yaw=1
gyro_precession_on_yaw=1
gyro_precession_on_pitch=1 
gyro_precession_on_roll=1

[weight_and_balance]

// ACM V2.5
max_gross_weight = 47398.6
empty_weight = 31261.02
reference_datum_position = -3.7, 0, 0
empty_weight_CG_position = 0.485, 0, 0
empty_weight_pitch_MOI = 400000
empty_weight_roll_MOI = 250000
empty_weight_yaw_MOI = 500000
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.88
CG_aft_limit = -0.7
//max_number_of_stations = 1

//station_load.0 =5318,-3.60542,0,0,Weight


max_number_of_stations = 36

station_load.0 =8746,-4.5055,0,0,Weight

[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 3, -2.26,-47.67, 3.24, fx_navredm ,
light.1 = 3, -2.26, 47.67, 3.24, fx_navgrem ,
light.2 = 2,-33.83,  0.00, 9.21, fx_beaconb ,
light.3 = 2, -4.80,  0.00,-4.21, fx_beaconh ,
light.4 = 3,-45.80,  0.00, 4.00, fx_navwhi  ,
light.5 = 4, 24.00,  2.00, 2.00, fx_vclight ,
light.6 = 4, 24.00, -2.00, 2.00, fx_vclight ,
light.7 = 5,  1.70, 26.42, 3.70, fx_landing ,
light.8 = 5,  1.70,-26.42, 3.70, fx_landing ,

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.01 //0.88
min_throttle_limit = 0.0
engine.0 = 12.00, -12.956, 3.0
engine.1 = 12.00, 12.956, 3.0

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2
electric_pump = 0

LeftMain = 0.485, -10, 4.3, 330.22, 0
LeftAux = 0.485, -17.4, 4.3, 486.08, 0
RightMain = 0.485, 10, 4.3, 330.22, 0
RightAux = 0.485, 17.4, 4.3, 486.08, 0


[contact_points]
static_pitch = -0.002
static_cg_height = 7
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 16

point.0 = 1.00, 22.70,     0.00, -7.30,  800, 0, 1.147, 60.0, 0.26, 2.5, 0.6, 4.50, 4.50, 0, 0, 0
point.1 = 1, -2.156, -12.4, -8.0, 1400, 1, 1.475, 0, 0.79, 2.5, 0.55, 4.5, 4.5, 2, 0, 0
point.2 = 1, -2.156, 12.4, -8.0, 1400, 2, 1.475, 0, 0.79, 2.5, 0.55, 4.5, 4.5, 3, 0, 0
point.3 = 2.00, 28.03,    -0.00, -4.90, 9000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 4, 0, 0
point.4 = 2.00, -2.26,     0.00, -5.24, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 4, 0, 0
point.5 = 2.00,-41.05,     0.00, -1.00, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 9, 0, 0
point.6 = 2.00, -5.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.7 = 2.00, -5.22,    47.50,  3.43, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.8 = 2.00, -1.22,   -47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.9 = 2.00, -1.22,    47.50,  3.42, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.10 = 2.00,  2.70,   -12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.11 = 2.00,  2.70,    12.50, -1.30, 6000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.12 = 2.00,-38.05,     0.00, 20.00, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0
point.13 = 2.00,-32.80,     0.00,  9.00, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0
point.14 = 2.00,  4.45,     0.00,  5.50, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 7, 0, 0
point.15 = 2.00, 24.20,     0.00,  3.75, 3000, 0, 0.000,  0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 8, 0, 0


[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000


[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 780
wing_span = 95.8
wing_root_chord = 8.8
wing_dihedral = 0.000
wing_incidence = 0.0
wing_twist = 0.00
oswald_efficiency_factor = 0.705
wing_winglets_flag = 0
wing_sweep = 0.0
wing_pos_apex_lon = 2.20
wing_pos_apex_vert = 4.3
htail_area = 185.461
htail_span = 29.823
htail_pos_lon = -36.5
htail_pos_vert = 3.000
htail_incidence = -3.00
htail_sweep = 21.000
vtail_area = 192.4
vtail_span = 16.076
vtail_sweep = 25.000
vtail_pos_lon = -33.4
vtail_pos_vert = 3.0
elevator_area = 55.54
aileron_area = 65.87
rudder_area = 53.819
elevator_up_limit = 30.0
elevator_down_limit = 15.0
aileron_up_limit = 24.0
aileron_down_limit = 16.0
rudder_limit = 25.000
elevator_trim_limit = 80   //45
spoiler_limit = 57.3
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 27
generator_alternator_voltage = 28
max_generator_alternator_amps = 600
engine_generator_map = 1,1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 15, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 10
light_beacon = 0, 5, 10
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 10
light_panel = 0, 5, 10

[Flaps.0]
type=1
span-outboard=0.600
extending-time=16.000
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=1.0 
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0= 0.000,  0.0
flaps-position.1= 5.000,  0.0
flaps-position.2=10.000,  0.0
flaps-position.3=15.000,  0.0
flaps-position.4=20.000,  0.0
flaps-position.5=25.000,  0.0
flaps-position.6=30.000,  0.0
flaps-position.7=38.000,  0.0

[Flaps.1]
type=1
span-outboard=0.600
extending-time=6.300
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=0.2 
drag_scalar=0.1
pitch_scalar=0.05
flaps-position.0= 0.000, 0.0
flaps-position.1= 5.000, 0.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0.0

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0
[folding_wings]
wing_fold_system_type=4
fold_rates=0.075,0.075
[exits]
number_of_exits = 2
exit_rate.0 = 0.09                             ;Percent per second
exit_rate.1 = 0.2                              ;Percent per second

[Reference Speeds]
flaps_up_stall_speed=102.000 
full_flaps_stall_speed=82.800 
cruise_speed=215.000 
max_indicated_speed=292.000000
max_mach=0.650000

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1, 0 
Com.2=1, 0 
Nav.1=1, 0, 1 
Nav.2=1, 0, 1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[autopilot]
autopilot_available=0 
flight_director_available=0 
default_vertical_speed=1000.000000 
autothrottle_available=0 
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000 
use_no_default_bank=0	//For no wing leveler when AP On
use_no_default_pitch=0	//For no pitch holding when AP On
autoland_available=0

[brakes]
toe_brakes_scale=0.518815
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=55.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[pitot_static]
vertical_speed_time_constant = 1.0   //0.7

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Views]
eyepoint=22.2, -1.70, 2.1 

[direction_indicators]
direction_indicator.0=3,0 

[main]
Pilot=1,80
CoPilot=1,80
Navigator=1,80
RadioOperator=1,80
FrontBaggage=1,250
FrontBaggageA=1,250
Dress=1,50
BackBaggage=1,50
Stewardess=1,80
Food=1,40
Rows.4=1,75,1,75
Rows.5=1,75,1,75
Rows.6=1,75,1,75
Rows.7=1,75,1,75
Rows.8=1,75,1,75
Rows.9=1,75,1,75
Rows.10=1,75,1,75
Rows.11=1,75,1,75
Rows.12=1,75,1,75
Rows.13=1,75,1,75
Rows.14=1,75,1,75
Rows.15=1,75,0,75
Rows.16=0,75,0,75
Rows.17=1,75,1,75
Rows.18=1,75,1,75
Rows.19=1,75,1,75
Rows.20=1,75,1,75
Rows.21=1,75,1,75
Rows.22=1,75,1,75
Rows.23=1,75,1,75
Rows.24=1,75,1,75
Rows.25=1,75,1,75
Rows.26=1,75,1,75
Rows.27=1,75,1,75
Rows.28=0,75,1,75
Rows.29=0,75,0,75

45221-An-24-dyn-v5.25-oldviz.zip

Имя файла Дата Размер
An-24_dyn_v5.25_oldviz/dynamics/ 16.06.2012 22:07
An-24_dyn_v5.25_oldviz/dynamics/Aircraft.cfg 13.06.2012 03:25 12 KB
An-24_dyn_v5.25_oldviz/dynamics/Antonov An-24RV.air 13.06.2012 02:14 14 KB
An-24_dyn_v5.25_oldviz/licence_agreement.txt 16.06.2012 20:38 2 KB
An-24_dyn_v5.25_oldviz/readme.txt 16.06.2012 23:24 563 B
avsim_su.diz 17.06.2012 08:40 406 B
Итого: 28 KB
Dynamics v.5.25 for An-24RV old visual model (pack Samdim_An-24RV V2.1).
Link to the pack Samdim_An-24RV V2.1:
→ Size: 14 KB
→ Date: 14 years ago (17.06.2012 00:52)
→ Author: Александр Терентьев AKA Aless
→ Uploaded by: Aless (uploaded 4 files )
→ Approved by moderator: SLAVJAN
→ License: License file included in archive
→ Downloaded: 1143 time(s)