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#1
May 11th 09, 06:00 PM
posted to rec.aviation.soaring
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Spin recovery vs tail design
I would like to solicit comments on the question: Compared to a standard
tail configuration such as a 2-33 or Blanik L-13, does the initiation and recovery from a spin vary substantially in T-tail (ASK-21 type), all-flying (Phoebus) or V-tail (HP series) sailplanes? Really look forward to reading and learning. 
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