Hello Jimi,
some feedback. I have been fiddling around with the drag and flaps values. Here is what I have come up with so far.
- I have checked some of the flaps values you provided with references (page 127 of 902 on F18-ABCD-000.pdf) and changed them accordingly: Leading Flaps do NOT move full out when on the ground or approach, etc. They only do so in Auto mode. Have a look at the changes in the .cfg file I have included.
- The extending-time values seemed much too slow. From a youtube video someone linked here where they are tested pre-flight, it seems they can be moving very quickly.
- I have corrected the span-outboard values too, by adjusting values in relation to each other via visual comparison (e.g. measuring the pixels from a detailed sketch and a screen shot). They should be closer the the real deal now.
As a starting point for the performance (Vmax and drag) adjustments I have taken the default fsx drag coefficients (from within .air under 'Primary Aerodynamics' section 'Drag') and their relations to each other and made a series of tests concerning Vmax with different parasitic drag scalars (in .cfg file) representing different loadouts. As reference parasitic drag scalar values I took the ones from different CaptainSim D version loadouts, and adjusted the drag values inside the .air file accordingly to match Vmax at high altitude. You can test the results if you like for yourself. I have attached the latest .air and .cfg files. If do not want to adjust paths etc. you can work with this version here:
http://www.fsdreamteam.com/forum/index.php/topic,10839.0.html ('New FSXBA Hornet' version)
For better understanding of the calculations I have added a screen shot of them below. The results seem to be promising.
Performance (At Maximum Takeoff Weight) F/A-18C/D:
- Max level speed: More than Mach 1.8
- Max speed, intermediate power: More than Mach 1.0
- Acceleration from 460knots to 920knots at 35,000ft: under 2 min (35,000ft: 460knots = Mach 0.79 ; 920knots = Mach 1.59)
See references posted here:
http://what-when-how.com/military-weapons/fighters-military-weapons/http://www.fsdreamteam.com/forum/index.php?PHPSESSID=5igml7o8t6atmkmepmte2oadm4&topic=6944.435Some more feedback:
- really like the new AB effects, looks more realistic to me.
- C version model error: in Trainer & BA model, pilot's heads are not moving and are looking funny, something with the hair/helmet seems to be wrong.
- I really like to work with the D version, but the blue color on internal parts of cockpit and canopy error is annoying. DX10 error? I'm still working with P3D 1.4, DX9 is showing errors here too!
- wing_dihedral value changed, to compensate for wing flex. When the FA-18 is static on the ground a dihedral of 2.5 degrees can be recognized (anhedral really, wing tips facing downward). But in flight even with no g-loads the wing tips get slightly lifted a little and the wings look almost to be leveled out, so I opted to change this value for more flight dynamics realism because the simulator cannot compensate for wing flex, which is just a visual thing. But then shouldn't this value be slightly negative by default for the FA-18? What do you think? References:
http://msdn.microsoft.com/en-us/library/cc526949.aspxhttp://www.multiplyleadership.com/blog/wp-content/uploads/2012/01/Dihedral-Angle.pnghttp://previewcf.turbosquid.com/Preview/2014/05/25__00_39_09/F-18_Front_400x400.jpg5218b422-12ae-462e-a067-0372e7187e5eLarger.jpg(By the way, your visual wing flex effect is awesome!)
- A few posts before I suggested a change of the wing sweep to 26.7 degrees which is obvious, but I ever wondered why the original developers had chosen 20 degrees? Now I found a source mentioning the Hornets wing sweep being "20° sweep at the quarter-chord". See here:
http://what-when-how.com/military-weapons/fighters-military-weapons/Especially with the LERXs' considered, in order to represent correct flight dynamics, I still would suggest a more 'realistic' assumed wing sweep of 26.7 degrees in the simulator being closer to the real deal than the originally choosen 20 degrees. But at least we know now where they got this number from, and I think I know why. When you take a 747 for instance, large parts of the leading edge flaps extract from inside and under the wing, changing the wing sweep over all during an approach, so when trying to compare airliners' wing sweeps it is being measured at the quarter-chord. But since the FA-18 does not extract and retract flaps that way and considering LERXs' I would go here with 26.7 degrees. In a Hornet A/B, C/D, E/F comparison (
http://www.dept.aoe.vt.edu/~mason/Mason_f/FA18.pdf ) 26.7 degrees for wing sweep (for C/D versions) are stated too. I hope this cleared things up.
- As for the design g load tolerances 8.0 vs. 7.5 I have read somewhere that the 8.0 were newer structurally enhanced wings/fuselage components compared to the older original ones, which can be retrofitted, but I cannot remember the source right now. I personally will stick with the 8.0 values here.
Thanks for the valuable thoughts concerning the landing gear values mentioned above, I will adjust them as soon as I get to it.
Best regards,
Peter