Dave Perry
2006-02-21 02:40:14 UTC
Some questions concerning YASIM and constant speed props (from flying
the pa24-250):
1. At manifold pressures below 20 in. hg, the pa24-250 has much too much
power compared to the real AC. I normally use 16 in of manifold
pressure in procedure turns and then with the gear down and 15 deg. of
flaps, the descent and airspeed fall in place at the outer marker. I
can't even carry 10 in MP in the yasim model in an approach.
2. A likely related issues is that with the prop all the way "forward"
(normal landing procedure), the RPM stays high at 85 mph and no throttle
as I flare out. In the real AC, the engine cannot keep the prop at high
RPM in this situation. This makes taxiing require a lot of braking or
you can pull the prop back, again not real. Also, parked, with the prop
"forward" and no throttle, the RPM builds to perhaps 1800 RPM. The
normal engine run-up is to 2000 RPM and getting it there requires nearly
20 in. hg MP. Again not realistic. Any suggestions form others using
yasim with a constant speed prop.
3. The cruise speeds are very nearly correct if I lean at altitude to
the proper fuel flow. If I leave the mixture rich, the speeds at
altitude are too high. The egt does not help me peak lean as leaning
does not change the egt value. Have I tied the egt to the wrong property?
I have thought that yasim did not handle constant speed props well
before when I could not get the p51 to slow up with the prop forward and
little or no throttle. I don't know if I can help tweak this. I have
done only a little little C++ programing. Most of my programming has
been numerical analysis in Fortran and C.
Willing to try,
Dave Perry
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the pa24-250):
1. At manifold pressures below 20 in. hg, the pa24-250 has much too much
power compared to the real AC. I normally use 16 in of manifold
pressure in procedure turns and then with the gear down and 15 deg. of
flaps, the descent and airspeed fall in place at the outer marker. I
can't even carry 10 in MP in the yasim model in an approach.
2. A likely related issues is that with the prop all the way "forward"
(normal landing procedure), the RPM stays high at 85 mph and no throttle
as I flare out. In the real AC, the engine cannot keep the prop at high
RPM in this situation. This makes taxiing require a lot of braking or
you can pull the prop back, again not real. Also, parked, with the prop
"forward" and no throttle, the RPM builds to perhaps 1800 RPM. The
normal engine run-up is to 2000 RPM and getting it there requires nearly
20 in. hg MP. Again not realistic. Any suggestions form others using
yasim with a constant speed prop.
3. The cruise speeds are very nearly correct if I lean at altitude to
the proper fuel flow. If I leave the mixture rich, the speeds at
altitude are too high. The egt does not help me peak lean as leaning
does not change the egt value. Have I tied the egt to the wrong property?
I have thought that yasim did not handle constant speed props well
before when I could not get the p51 to slow up with the prop forward and
little or no throttle. I don't know if I can help tweak this. I have
done only a little little C++ programing. Most of my programming has
been numerical analysis in Fortran and C.
Willing to try,
Dave Perry
-------------------------------------------------------
This SF.net email is sponsored by: Splunk Inc. Do you grep through log files
for problems? Stop! Download the new AJAX search engine that makes
searching your log files as easy as surfing the web. DOWNLOAD SPLUNK!
http://sel.as-us.falkag.net/sel?cmd=lnk&kid=103432&bid=230486&dat=121642