Postby Phil Clark » February 2nd, 2014, 11:41 pm
Hi Carl
From all the research I have done, and people I have spoken to who have built & flown large 335's, it appears you have to run more pitch on the rear prop than on the front. There is a lot to it, but the simple explanation seems to be that because both engines are 'in line'......the air hitting the rear prop has already been accelerated/turbulated by the front prop, so if you have identical pitch on the rear to that of the front prop, it'll have little effect and create drag rather than thrust, hence if it were me, I'd be looking at something like a 26" x 14" on the rear.
I cannot confirm exactly what was done on the full-size, but I'm pretty sure I'm right in saying the 2 props were not the same (can check tomorrow when back at work). They varied in diameter which would suggest different pitches were used front to rear.........but considering both engines were the same, it points more towards 2 different props than 2 identical.
Re:- Cooling.......I have air entering the fuselage via both supercharger scoops, plus the large scoop under the rear fuselage. My exit area consists of the 2 large flaps under the stab (approx. 1" x 3"), a smaller one on the underside of the fuz ahead of the lower fin (approx. 2" x 1/2") plus through the rear fuz through slots in the rear former carrying the rear bearing housing. All of these are rear facing so forward movement & airflow passing back along the surface of the fuz will basically scavenge hot air out from inside the fuz. I have no internal cooling fan, but the main internal bulkhead the rear 45 is mounted to has a hole in it approx. 3" square directly in front of the cooling fins........this will be ducted so any air entering the fuz ahead of this bulkhead has to pass through said hole & through the cooling fins when flowing through to the rear fuz and the exit openings.
This is a proven kit and the system works. I have a customer with this kit over in Texas where it's VERY hot and he's had no overheating issues.......he has carried outs temp test and it shows the rear engine runs cooler (approx. 20 deg IIRC) with the front engine running, compared to it stopped, so the rearward airflow created by the front engine forcing air into the inlet openings & through the fuz I definitely having an effect.
Re:- weight.......what's she come in at?......and what's the wing loading.
Phil