Adam Day wrote:

>>My question is does any on here have a KR based at high altitude or 
>>frequently go above 10,000 feet ? and if so what engine are you using and 
>>how
the plane handles, climb and cruise with a given prop?<<

I do most of my flights at 9500-10500 feet, and I've been over 20,000' once, 
just to see where the ceiling was.  It was still climbing, but not much. 
You really can't tell the difference in the way it handles at higher 
altitudes (within reason), as indicated airspeed appears the same to the 
pilot as it does to the plane, if that makes sense.   As Jeff mentioned, 
diminished climb rate is the problem, but it's still better than a lot of 
spam cans.  You probably wouldn't want to fly behind an 1835cc VW at those 
altitudes, just as a matter of safety (climb performance), but I'm sure 
somebody out there would disagree.  I guess that's subjective, but you can 
hang numbers on the climb rate, and that does matter from a 
"return-to-the-field" standpoint.

Altitude has an almost direct relationship with engine power, so at 8000' 
you start out with 75% engine power, not to mention reduced lift.  There's a 
nice chart at http://www.cobham.com/media/83823/821-1.pdf that quantifies 
the pressure (and therefore performance) difference at altitude.  I have a 
plastic water bottle that I opened at 17,000', emptied, and then resealed. 
After landing I noticed it looked like it'd been flattened.  It had 
collapsed inward, and looks like 2/3 of the volume is gone from it now. 
That's a powerful reminder of the effects of high altitude.  Note that I 
have an oxygen cylinder and use it, as does Joe Horton and some other 
high-flyers on this list.  Joe could tell you a story about what happens 
when you run out of oxygen and don't realize it, but that might have to wait 
until a few beers and the campfire at the Gathering in September!

One of the design parameters for the AS504x airfoil was the same lift 
coefficient as the RAF48, so if the wing area is the same on the new wing as 
the old one, lift should be the same.  Lower drag is the "free lunch" 
benefit.  Having over 1100 hours on the new wing, I highly recommend it as 
now "proven"...

Mark Langford
ML at N56ML.com
website at http://www.N56ML.com
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