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To add to the confusion:
Many modern gliders are elevator limited - full aft stick just won't result in enough AOA to stall the wing. Nothing to do with the tail being stalled. In fact, it's "lifting" just fine, just in the "down" direction (which could be up if you are at the top of a loop). If the tail did actually stall, you would get a brisk nose down pitch rate, I would think! It would be almost the same as the horizontal tail falling off. Think about it.... Also, the tail on modern gliders do not always push "down". Depends on speed, AOA, G-load, CG location, flap position, etc. You have to look at the entire lifting contributions of all the parts of the glider. Stability is due more to decalage. Look it up. It's amazing how little most pilots know about how their aircraft really work....including yours truly! Kirk 66 |
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