Toobuilder
Well Known Member
...Started this thread to avoid corrupting the other "ballast" thread...
Yes, this has been beat to death, but the answers I have found so far are not what I'm looking for.
Therefore, with the generally accepted fact that "all" RV-8's are nose heavy when solo and fly "better" with the C/G moved aft, what is the point where it flies "good"? Before someone talks about battery location, angle valve, prop type, etc, understand that the only bit of info required is the actual C/G (or %MAC) that results in "good" flying for the RV-8 airframe. In other words, there is a point with some combination of ballast, baggage, fuel, ect that "feels" good... This same point also has an instantaneous (loaded) C/G of some value, and (for like aircraft, in this case the -8) this value is independent of total weight, where the battery is, prop type, or what color the airplane is painted.
So the question is: What is the best "loaded" solo C/G value?
Yes, this has been beat to death, but the answers I have found so far are not what I'm looking for.
Therefore, with the generally accepted fact that "all" RV-8's are nose heavy when solo and fly "better" with the C/G moved aft, what is the point where it flies "good"? Before someone talks about battery location, angle valve, prop type, etc, understand that the only bit of info required is the actual C/G (or %MAC) that results in "good" flying for the RV-8 airframe. In other words, there is a point with some combination of ballast, baggage, fuel, ect that "feels" good... This same point also has an instantaneous (loaded) C/G of some value, and (for like aircraft, in this case the -8) this value is independent of total weight, where the battery is, prop type, or what color the airplane is painted.
So the question is: What is the best "loaded" solo C/G value?
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