Re: yasim and constant speed props??
Lee Elliott <[email protected]> Tue, 21 Feb 2006 19:09:43 +0000
| Newsgroups | gmane.games.flightgear.flightmodel |
|---|---|
| Message-ID | <[email protected]> |
On Tuesday 21 February 2006 02:40, Dave Perry wrote: > 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 Hello Dave, I don't know if this helps but while messing around with the TU-114 I found that if I omitted the control _input_ axis for the prop pitch I could then see the prop pitch changing as airspeed increased. Unfortunately though, the pitch seemed to start at 0.48 and dropped to 0.0 by a couple of hundred knots ias. This is most likely due to me mis-configuring the props as it's not something I know much about. If I included the control input for the prop pitch then the pitch seemed to stay set at whatever was specified - no constant-speed effect. LeeE ------------------------------------------------------- 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