Brett_Henderson wrote on Dec 11
th, 2008 at 7:05am:
Lastly, edit the paint-job to have "EXPERIMENTAL" posted clearly near both doors.. And edit the panel bitmaps with a similar warning..
The paint shop is WAAAY ahead of the mechanics on this project.
http://i34.tinypic.com/2e4wy93.jpgI'm not a pilot, so this all an exercise for my entertainmentand I am looking to replace the the AEIO-360-A1D configuration for an AEIO-540-K1A5.
I made changes to cylinder displacement, HP and compression ratio. I also changed the pitch range of the prop so that it does not run over 3K. I have adjusted the aircraft weights by an additional 137 lbs and will be looking at the aircraft body model later to look for the additional 10" I'll need for the length of the motor. I was considering reducing the fuel available to offset the engine weight.
It's a wild ride as it is... throttle touch has to be light or it runs away with you. The IAS pegs at 230 and will fly there a LONG time before the craft comes apart. The "never exceed" speed in the reference is 210 so it feels unrealistic. Can I bump this so that overspeed causes tragic results sooner? What else? How is fuel consumption calculated? Should I change props? Stay with the constant speed or change to a fixed pitc? Two blades? Three? Where can I adjust for the effects of torque in the config file? Will Luke and Laura ever find true happiness together?
Here is where I am so far, I really appreciate you taking the time to look. Happy flying!
Rick
[piston_engine] // LYC AEIO-540-K1A5
power_scalar = 1.0 // Six-cylinder air-cooled horizontally opposed engine
cylinder_displacement = 130 //90 Bore: 5.125 in
compression_ratio = 10 //original: 8.7 Stroke: 4.375 in
number_of_cylinders = 6 //6 Displacement: 541 cu in
max_rated_rpm = 2700 //original: 2700 Weight: 440 lb
max_rated_hp = 322 //200
fuel_metering_type = 0
cooling_type = 0
normalized_starter_torque = .32
turbocharged = 0
max_design_mp = 0 //29.9
min_design_mp = 0 //9
critical_altitude = 0
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
emergency_boost_duration = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1
[propeller] // Hartzell 81HC-C2YK-4CF/FC7666A-2 constant speed prop
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 6.1
propeller_blades = 2
propeller_moi = 3.4
beta_max = 50 //original: 65
beta_min = 15 //original: 15
min_gov_rpm = 405
prop_tc = 0.01
gear_reduction_ratio = 1
fixed_pitch_beta = 25
low_speed_theory_limit = 77.1402982083445
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available = 0
prop_auto_feathering_available = 0
min_rpm_for_feather = 700
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = 1