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#18
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On Jan 26, 5:57*am, mart wrote:
Now the problems started. While putting the airbrakes away the flaps slipped to negative. *Not very handy at 20 feet and relatively slow. The glider promptly stalled. He than did what he was thought by a test pilot." If everything goes to ****, reverse the last thing you have done." So contrary to what you would normally do when stalled, which is to push the nose over , he pulled the brakes again, which in turn pulled the flaps out again. He said that it saved his bacon. Took out the undercarriage and hurt his back, but he walked away. Mart I am surprised that only one pilot responded to the misconceptions exibited it the above post! I tried to respond but for some reason my posts don't seem to get throught... Anyway, the misconception is that sudden retraction of flaps will cause a "stall". And in the case above, that a "non-stall recovery", "recovered the glider from a stall". Retracting flaps will DECRERASE the effective angle of attack. If the glider was not already stalled, DECREASING the angle of attack certainly will not stall it. What the sudden flap retraction did however, is change the coeffecient of lift, which resulted in an imbalance of lift, drag and weight, which in turn resulted in an acceleration, which was partly DOWNWARD.... The pilot simply redeployed the flaps, returning the original coeffecient of lift, which arrested the downward acceleration. A non-stall recovery, for a non stall problem! The pilot could have also pulled back on the stick, which might have restored the balance of lift, drag, and weight, and arrested the high sink rate. This however, WOULD increase the angle of attack, and might possibly cause an actual stall if the critical angle was exceeded. Cookie |
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