@Bill
Below are cutouts from the original .cfg
Comparing the bold printed values of W8 and W10, I can see only slight differences in displacement but none in weight and prop. What do I misunderstand here?
W10
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 85.75 //Cubic inches per cylinder
compression_ratio= 7.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2300 //Max rated RPM
max_rated_hp= 65 //Max rated HP
fuel_metering_type= 2 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.56 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.78 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 1220 // (pounds)
empty_weight = 680
[Reference Speeds]
flaps_up_stall_speed=65.0 //Knots True (KTAS)
full_flaps_stall_speed=49.0 //Knots True (KTAS)
cruise_speed=150.0 //Knots True (KTAS)
max_indicated_speed=190.0
W8
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 73.75 //Cubic inches per cylinder
compression_ratio= 7.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2300 //Max rated RPM
max_rated_hp= 65 //Max rated HP
fuel_metering_type= 2 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.53 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.78
[WEIGHT_AND_BALANCE]
max_gross_weight = 1220 // (pounds)
empty_weight = 680 // (pounds)
[Reference Speeds]
flaps_up_stall_speed=65.0 //Knots True (KTAS)
full_flaps_stall_speed=49.0 //Knots True (KTAS)
cruise_speed=150.0 //Knots True (KTAS)
max_indicated_speed=190.0
Mike
Below are cutouts from the original .cfg
Comparing the bold printed values of W8 and W10, I can see only slight differences in displacement but none in weight and prop. What do I misunderstand here?
W10
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 85.75 //Cubic inches per cylinder
compression_ratio= 7.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2300 //Max rated RPM
max_rated_hp= 65 //Max rated HP
fuel_metering_type= 2 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.56 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.78 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 1220 // (pounds)
empty_weight = 680
[Reference Speeds]
flaps_up_stall_speed=65.0 //Knots True (KTAS)
full_flaps_stall_speed=49.0 //Knots True (KTAS)
cruise_speed=150.0 //Knots True (KTAS)
max_indicated_speed=190.0
W8
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 73.75 //Cubic inches per cylinder
compression_ratio= 7.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2300 //Max rated RPM
max_rated_hp= 65 //Max rated HP
fuel_metering_type= 2 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar = 0.53 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.78
[WEIGHT_AND_BALANCE]
max_gross_weight = 1220 // (pounds)
empty_weight = 680 // (pounds)
[Reference Speeds]
flaps_up_stall_speed=65.0 //Knots True (KTAS)
full_flaps_stall_speed=49.0 //Knots True (KTAS)
cruise_speed=150.0 //Knots True (KTAS)
max_indicated_speed=190.0
Mike