Robert,
I am hoping to run a test flight with it next week, weather hasn't cooperated here lately, too much gusty wind for accurate data collection.
The first test was done not at the desired pitch setting but for numbers the following was found. at 33.3* pitch 3 blade 160CM.
Density altitude for takeoff 4200'
Static RPM 5630
From start of takeoff roll, I took 7 seconds to feed in full throttle, by that time I was doing 30 KTS IAS and RPM was down to 5573 MAP was 27.1 Hg
5 seconds later 42KTS and 5526 RPM MAP was 27.1
6 seconds later 50 KTS and 5475 RPM MAP still 27.1 Airborne now
3 seconds later 61 KTS and 5380 RPM MAP 27.1 VSI plus 550
76 KTS has RPM at 5250 MAP 27.1
87 KTS has RPM at 5186 MAP 26.9
100 KTS has RPM at 5141 MAP 25.3
110 KTS has RPM at 5221 MAP 25.0
120 KTS has RPM at 5240 MAP 23.5
125 KTS has RPM at 5400 MAP 23.5
130 KTS has RPM at 5452 MAP 23.2
Density altitude was now 8200' and not able to maintain above 125 KTS IAS without slight decent.
Climb performance shown between 800' and 1000' VSI all the way up to this density altitude.
As you can see, at no point does the RPM go above static and gets slower as you increase airspeed up to 100 KTS IAS. Above that it starts to unload again but still close to 200 RPM below static. I adjusted the pitch again to increase the LFWOT to 5550 which should be ideal and will run more testing once ideal RPM is achieved.
Here are some pictures of the prop but no top cowl on. I will get better pics next time out there.
- Eprop1.jpg (178.15 KiB) Viewed 3254 times
- Eprop2.jpg (194.08 KiB) Viewed 3254 times
- Eprop3.jpg (231.77 KiB) Viewed 3254 times