[fltsim.0]
title=Blanik L-13 Front
sim=Blanik
model=
panel=
sound=
texture=
texture=
kb_reference=Blanik_ref
kb_checklists=Blanik_check
ui_manufacturer=Let/Czechoslovakia
ui_type=Blanik L-13
ui_variation=Front Seat
description= The Czech two-seater Blanik L-13 is one of very few gliders of all-metal construction.
[General]
performance=Length: 8,40 m\nWing span:16.20 m\nWeight:292 kg empty, 500 kg all up\nDetails: Best gliding ratio 1:28 \/ 86 km\/h \nMinimum sink rate 0.85 m\/s \/ 68 km\/h \nVNE: 280 km\/h\nDesigner: Wolfgang Piper\nGauges: Max Roodveldt\nDate:Oct. 2004
[electrical]
max_battery_voltage=24
avionics_bus=0, 0 , 0
avionics=0, 0 , 0
additional_system=0, 0 , 0
flap_motor=0, 0 , 0
gear_motor=0, 0 , 0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[WEIGHT_AND_BALANCE]
max_number_of_stations=5
reference_datum_position=0.0000000,0.000000,0.000000
station_load.0="170, 4.0,0,0,Pilot"
station_load.1="170, 0, 0,0,Guest"
empty_weight=644.000000
empty_weight_roll_MOI=2200.000000
empty_weight_pitch_MOI=2000.000000
empty_weight_yaw_MOI=800.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=1102.000000
empty_weight_CG_position=-2.0000000,0.000000,0.000000
[flight_tuning]
cruise_lift_scalar=1.2
parasite_drag_scalar=0.78
induced_drag_scalar=1.06
elevator_effectiveness=0.90
aileron_effectiveness=0.8
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.2
yaw_stability=1.0
elevator_trim_effectiveness=1.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[airplane_geometry]
wing_area=190.000000
wing_span=53.0
wing_root_chord=5
wing_dihedral=0
wing_incidence=1.0
wing_twist=1.999512
oswald_efficiency_factor=0.875082
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.500000
wing_pos_apex_vert=1.000000
htail_area=25.000000
htail_span=6.333333
htail_pos_lon=-16.416667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=32.000000
vtail_span=6.449806
vtail_sweep=0.000000
vtail_pos_lon=-14.750000
vtail_pos_vert=3.916667
elevator_area=13
aileron_area=11.900000
rudder_area=7.700000
elevator_up_limit=27
elevator_down_limit=15
aileron_up_limit=17
aileron_down_limit=10
rudder_limit=23.491270
elevator_trim_limit=35
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[contact_points]
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
// Lang. Breit. Vert.
// Pos. Pos. Pos.
// 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
//--------------------------------------------------------------------------------------------------------------------------------
point.0 = 1, -19.0, 0.0, -1.11, 1500, 2, 0.5, 0, 0.2, 1.5, 0.8, 0, 0.5, 4, 0, 0 // Gear Tail
point.1 = 1, 1.2, -0.5, -3.60, 1500, 1, 0.85, 0, 0.2, 2.0, 1.0, 0.5, 0.5, 3, 0, 0 // Gear Main
point.2 = 1, 1.2, 0.5, -3.60, 1500, 2, 0.85, 0, 0.2, 2.0, 1.0, 0.5, 0.5, 3, 0, 0 // Gear Main
point.3 = 1, 4.0, 0.0, -2.60, 1500, 2, 0.4, 0, 0.4, 2.5, 0.8, 0.5, 0.5, 3, 0, 0 // Gear Nose
point.4 = 2, 5.6, 0.00, -2.6, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0//scrape front
point.5 = 2, -18.750, 0.00, -0.543, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0//scrape rear
point.6 = 2, 0.000, 26.198, 2.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0//wing
point.7 = 2, 0.000,-26.198, 2.00, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0//wing
static_pitch=4
static_cg_height=3.60
//gear_system_type=0
gear_system_type=0
[Views]
eyepoint= 2.76, 0.00, 0.5 //Front Seat
//eyepoint= -.5, 0.00, 0.8 //Rear Seat
[Reference Speeds]
flaps_up_stall_speed=32.000000
full_flaps_stall_speed=30.000000
cruise_speed=45
max_indicated_speed=152.734375
max_mach=0.229980
[keyboard_response]
elevator=100.000000,150.000000
aileron=100.000000,150.000000
rudder=100.000000,150.000000
[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available=0
flight_director_available=0
[direction_indicators]
direction_indicator.0=0,0
[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5#
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1#
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[brakes]
toe_brakes_scale=1.000035
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=1.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=4,0.000000
flaps-position.2=8,0.000000
flaps-position.3=12,0.000000
flaps-position.4=16,0.000000
flaps-position.5=18,0.000000
lift_scalar = 1.4
drag_scalar = 2.50
pitch_scalar= 1.0
system_type = 3
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[fuel]
fuel_type=1.000000
[GeneralEngineData]
engine_type=2
fuel_flow_scalar=1.000000