green66
Jul 15, 2002, 06:24 PM
Flew my Organic glider with CG 40% behind LE (35% is mfr's position). The plane was slightly tail-heavy: 1) squirrely in yaw, 2) tendency to tuck at high speed, 3) hard to establish pitch trim, 4) generally an effort to maintain straight & level.
So I added about 1/2 oz to the nose to shift the CG forward.
On the next flight, the plane was so (seemingly) tail-heavy that there wasn't nearly enough down-trim on the tx to compensate. I tried to hold down elevator to maintain control, but it went into a spiral dive (fortunately into tall brush, but didn't come out unscathed :( )
As far as I'm aware, the only thing that changed between the two flights was the added nose weight - no loose internals to shift around, no misaligned or damaged wing/tail panels, no control changes, etc.
Question - Could this "reversed" (going against expectation) effect of the changed CG have anything to do with the plane being near a neutral stability condition? Any explanations?
It's not the damaged plane that bugs me as much as not having a clue what caused the crash :confused:
So I added about 1/2 oz to the nose to shift the CG forward.
On the next flight, the plane was so (seemingly) tail-heavy that there wasn't nearly enough down-trim on the tx to compensate. I tried to hold down elevator to maintain control, but it went into a spiral dive (fortunately into tall brush, but didn't come out unscathed :( )
As far as I'm aware, the only thing that changed between the two flights was the added nose weight - no loose internals to shift around, no misaligned or damaged wing/tail panels, no control changes, etc.
Question - Could this "reversed" (going against expectation) effect of the changed CG have anything to do with the plane being near a neutral stability condition? Any explanations?
It's not the damaged plane that bugs me as much as not having a clue what caused the crash :confused: