bvolcko38 wrote:At our low rpm 3000 +/-, why do we need dual ports and bigger valves. This is for high rpm power, no?
DCASonex wrote:Hambone, Kia is right, you have been flying alone. Find your local EAA chapter, Closest here is about 65 mile drive, but elected to join one about 85 miles from here. For the right group pf people, it is worth the longer drive. so if you have options, check out more than one local.
One way or the other life is one long learning experience. Enjoy the ride.
David A.
Bryan Cotton wrote:bvolcko38 wrote:As I see it, the elephant in the room is Chinese parts made of Chinese materials.
Amen!
DCASonex wrote:Hambone, Kia is right, you have been flying alone. Find your local EAA chapter, Closest here is about 65 mile drive, but elected to join one about 85 miles from here. For the right group pf people, it is worth the longer drive. so if you have options, check out more than one local.
One way or the other life is one long learning experience. Enjoy the ride.
David A.
Hambone wrote:Thanks for the wealth of advice and experience. I’m taking it all on board as I contemplate the way forward.
Edit: I’m certainly intrigued by the variety of heads on offer. I have a buddy who is an air-cooled VW specialist, albeit non-aviation. I’ll seek his advice, too.
Kai wrote: ...pressure differensial cooled VW-1 aeroderivatives have almost no cooling at all!
pfhoeycfi wrote:Fyi something to consider. I measured the cooling air PD across the engine from above the engine to near the right side exit.
The values were...at IAS
2" at 65 mph
2.5" at 75 mph
3" at 85 mph
3.5" at 95 mph
4" at 100 mph
4.5" at 110 mph
5" at 120 mph
I used an old school manometer and my IAS is what it is. The values are rounded. Another airplane will likely have different results. But its a baseline. Attempts at flow improvements will yield greater (hopefully), the same or lower DPs at these speeds. I'll likely confirm the numbers before I make any changes. I'm also going to check the DP across the oil cooler.
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