TAS/GS weirdness
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@BernieV Another data point that the drag in the climb is too low is that I was able to climb to 20,000 ft in the 0.2.0 model with the tweaks I made to parasitic drag and fuel flow (albeit at less than gross weight). I barely made it to 13,000 on a hot day between Napa CA and Yellowstone in real life and book shows 15K as the service ceiling. So now I am looking for a way to slow the climb and reign in the service ceiling (hopefully with a single parameter!)
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I appreciate all the research and testing you're doing, Bernie. I've noticed the Archer is running slower than I thought it should be -- a friend suggested maybe it was because they modeled the 3-blade prop instead of the 2-blade prop. I don't have the real world experience on the Archer to really add to or comment on it beyond that.
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@piedmonitor Whatever they modeled, we all agree that the numbers should match to the ODM that is included in the addon, don't we?
I also doubt that the 3-blade version isn't capable of a 75% power cruise no matter what the TAS is that results for that version. So there is definitely some issue with the flight model and I hope that someone from JF Staff is reading these findings and the devs are looking into it. -
Thanks for these tweaks. I noticed similar discrepancies with Little Navmap.
On the 25/25 rule, not everyone agrees. Came across this recently. See in particular John Collins’ comment and subsequent discussion.
https://www.pilotsofamerica.com/community/threads/the-25-25-myth.74115/
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@j225 said in TAS/GS weirdness:
Thanks for these tweaks. I noticed similar discrepancies with Little Navmap.
On the 25/25 rule, not everyone agrees.
Agreed. I think that 25X25 is specified in my POH (for a '67 Arrow, not a III like this model, but pretty close in most aspects and both have 4 cylinder IO-360s engines) for climbs, but I get your point. Get a bunch of pilots together on a non-flying day, add a few adult beverages, and mention either lean-of-peak operations or he "right" combination of MP & RPM for a given engine, and watch the fur fly ;) I think the conversation you referenced managed to work both topics into the conversation!
I've put 1850 hours on my engine since rebuild and compressions are still good, so I'll stick with what got me this far. Fingers crossed and hoping to get to 2000 hours on this engine. The nice thing with a sim is you can do whatever you like and you wont have to pull out your wallet and pay for a top end overhaul or rebuild.
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I've done one more round of testing and have have achieved a good balance of 75% power cruise TAS , climb performance, airspeed buildup in the descent, and service ceiling. They are as close to book at I can get for now.
In flight_model.config
parasite_drag_scalar =0.8
induced_drag_scalar =1.88In engines.config
fuel_flow_scalar =0.73
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@BernieV , Thanks for doing this research, and the recommended settings for achieving more realistic performance. For reference, the Parasitic Drag of any aircraft (parasite_drag_scaler) affects both the cruise speed and climb performance, while the Induced Drag (induced_drag_scaler) affects mainly the climb performance. The speed and climb performance are both determined by the ratio of Total Thrust vs. Total Drag of the aircraft...
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@RetiredMan93231 You are welcome RetiredMan. In practice, the induced drag scalar was the parameter that tuned rate of climb, the "slipperiness in the descent" (not a book value, but one I know from experience), and service ceiling. The final values posted gave me 137 kts level cruise at 75% power at 6500 ft (FT, 12 g/h, 2500 rpm as per book), an increase in TAS of 10 kts in a 500 ft descent at 75% power out of 6500 ft (from experience I expect 15 kts pickup, but I didn't want to detune ceiling or rate of climb for this subjective performance metric), and a service ceiling of 15000 ft (book).
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@BernieV , In the real world Arrow III what is the expected RPM / power level on final at 75 knots with full flaps? It seems to me that the landing gear drag and the flaps drag are both currently a little too high, requiring too much power (RPM) to maintain the glideslope on final. What are your thoughts?
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@RetiredMan93231 Between 15 and 17 inches of MP, prop level full forward, mixture full rich (unless operating at high elevations)
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@set3times No problem. The last (3rd) notch of flaps is almost all drag. In real life, I delay using it until I am sure I'd make the airport if I lost power or unless I was high/fast on the approach and need to get down or slow down.
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@BernieV Just tested your settings and it feels SO much better now :) Thank you for your research, I can only imagine how much effort that is.
Let's see what JF brings in a future update, but until then I'll be using your setup! The EGT is a bit odd but I'll go with the fuel flow gauge, as you said. That works fine.
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I have tested those values but I have an excessive RoC at around 1300fpm at 90knots at 2200lbs. (sea level)
EDIT: I just noticed I had a rapid headwind increase during initial climb-out, so disregard last transmission, will test in calm conditions ;)
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Tested in calm conditions with the values mentioned by BernieV but I find the RoC way too high (above 1200fpm) with full throttle and full prop (these are the values used in the performance manual reference, they might not be used in reality but that's the only reference we have).
