B5N1 中島九七式艦上攻撃機 (CFS2Default/AI)

機種別の変更点をまとめておきます。
※導入方法は『CFS2機体の導入方法』により詳しく記載してあります。

 

 

 

 

 

1.Airファイル

①元々AI機なので、Airファイル105番のAircraft Type=2をAircraft Type=0に変更。

②1101番、Primary Aerodynamicsのところ、
*lift-Flaps=0.000000を*lift-Flaps=0.400000に変更します。

③同様に *Pich Moment-Flaps=0.000000を*Pich Moment-Flaps=0.050000に変更します。

④変更後は『B5N2_Kate_ a』など名前を変えて保存することをお薦めします。

 

2.Aircraft.cfg

①Airファイル変更時に変更後のファイル名を別名とした場合、
適用するAirファイルを変更します。
また、機体の選択時に当該機種を表示させる為や、
ATCの為の記述を加えます。

//sim=B5N2_Kate
sim=B5N2_Kate_a 
   
//(*内容を変更したAirファイルを”B5N2_Katel_a.air”とした場合。)


////////////////////////////
ui_manufacturer=Nakajima
ui_type=B5N2
ui_variation=CFS2
description=nd

atc_id=JA9701
atc_airline=army
atc_flight_number=97
//////////////////////////////

エンジンのアイドリングが効かないようなので、
エンジン内の摩擦抵抗を少し減らします。
[piston_engine]セクション

//idle_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=0.700000

③フラップ関係の調整をフラップセクションに追加します。

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1
///////////////////////////////(//で囲まれた部分の追加)
lift_scalar= 0.7
drag_scalar= 1.0
pitch_scalar= 1.0
///////////////////////////////


④着艦フックとEFFECTSの追加をします。

////////////////////////////////////////////
[TailHook]
tailhook_length=4.5
tailhook_position = -17.2, 0.0, -1.5

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s,1
///////////////////////////////////////////////

⑤フライトチューニングによる変更を記述します。

//elevator_effectiveness = 1.0
elevator_effectiveness = 1.4
//pitch_stability = 1.0
pitch_stability = 1.8

 

3.PANELホルダー

中身が空なので、手持ちの汎用パネルを適用するか、他の機体のPANELを流用します。

 

4.SOUNDホルダー

sound.cfgの中身が[fltsim]alias=A6M2_Zero\soundのみとなっていますので、A6M2が無い場合、参照先を変更するか、SOUNDホルダーの中身を他の機体から流用します。

 

以上です。

 

**********************************
**********************************

 

記述例としてAircraft.cfgを記載しておきます

/////////Aircraft.cfg 例/////////////////////////

[fltsim.0]
title=B5N2 Kate
sim=B5N2_Kate
model=
panel=
sound=
texture=

ui_manufacturer=Nakajima
ui_type=B5N2
ui_variation=CFS2

atc_id=JA9701
atc_airline=army
atc_flight_number=97

description=nd

[WEIGHT_AND_BALANCE]
empty_weight = 5024.0 // (pounds)

reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = 170, 2.5, 0.0, 1.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -5.0, 0.0, 1.5 //Gunner Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI = 6436.81 //slug-ft^2
empty_weight_roll_MOI = 6325.35 //slug-ft^2
empty_weight_yaw_MOI = 10651.38 //slug-ft^2
empty_weight_coupled_MOI=0.000000
max_gross_weight=8046.000000

[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
//elevator_effectiveness = 1.0
elevator_effectiveness = 1.4
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
//pitch_stability = 1.0
pitch_stability = 1.8
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0

[piston_engine]
power_scalar = 1.0
cylinder_displacement=126.000000
compression_ratio=7.200000
number_of_cylinders=14
max_rated_rpm=2600.000000
max_rated_hp=985.000000
fuel_metering_type=0
cooling_type=0
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=39.999999
min_design_mp=1.000000
critical_altitude=10000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
//idle_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=0.700000//0.750000/0.800000

[propeller]
thrust_scalar = 1.0
propeller_type=0
propeller_diameter=10.500000
propeller_blades=3
propeller_moi=30.380000
beta_max=49.000000
beta_min=22.000000
min_gov_rpm=1400.000000
prop_tc=0.010000
gear_reduction_ratio=1.710000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0

[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
point.0=1, -22.84, 0.00, -1.73, 1600, 0, 0.25, 90.0, 0.30, 2.5, 0.90, 3.5, 3.3, 0
point.1=1, 0.96, -6.42, -6.65, 2200, 1, 1.25, 0.0, 0.50, 2.5, 0.79, 6.5, 7.5, 2
point.2=1, 0.96, 6.42, -6.65, 2200, 2, 1.25, 0.0, 0.50, 2.5, 0.79, 5.0, 7.0, 3
point.3=2, 0.00, -20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5
point.4=2, 0.00, 20.00, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6
point.5=2, -20.25, 0.00, -1.26, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9
point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4

static_pitch = 12.31 //degrees (pitch when loaded on ground)
static_cg_height = 5.82 //(feet) altitude of CG when at rest (altitude when loaded on ground)
gear_system_type=1

[Views]
eyepoint = -2.41,0.00,2.11 //(feet) longitudinal, lateral, vertical distance from reference datum




[General]
performance=Need specs here

[fuel]
LeftMain=-1.000000,-4.600000,-1.000000,145.000000,0.000000
RightMain=-1.000000,4.600000,-1.000000,145.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area=415.000000
wing_span=50.916667
wing_root_chord=8.083333
wing_dihedral=6.701660
wing_incidence=0.999756
wing_twist=0.000000
oswald_efficiency_factor=0.700361
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=24.000000
htail_span=11.000000
htail_pos_lon=-18.833333
htail_pos_vert=0.000000
htail_incidence=-0.999756
htail_sweep=0.000000
vtail_area=15.000000
vtail_span=4.415880
vtail_sweep=0.000000
vtail_pos_lon=-18.833333
vtail_pos_vert=0.583333
elevator_area=13.000000
aileron_area=20.400000
rudder_area=13.060000
elevator_up_limit=26.000825
elevator_down_limit=26.000825
aileron_up_limit=21.497376
aileron_down_limit=20.345731
rudder_limit=28.997394
elevator_trim_limit=19.996227
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1

/////////////////////////////////////////
lift_scalar= 0.7
drag_scalar= 1.0
pitch_scalar= 1.0
/////////////////////////////////////////

flaps-position.0=0.000000,0.000000
flaps-position.1=11.426415,0.000000
flaps-position.2=22.852831,0.000000
flaps-position.3=34.279246,0.000000
flaps-position.4=45.705662,0.000000
flaps-position.5=57.132077,0.000000
flaps-position.6=68.558493,0.000000
flaps-position.7=79.984908,0.000000

[GeneralEngineData]
engine_type=0
Engine.0=8.750000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[Reference Speeds]
flaps_up_stall_speed=67.000000
full_flaps_stall_speed=53.600000
cruise_speed=194.748106
max_indicated_speed=760.500000

[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556

[stall_warning]
type=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0

//////////////////////////////////////////////
[TailHook]
tailhook_length=4.5
tailhook_position = -17.2, 0.0, -1.5


[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1


///////////////////////////////////////////////
以上