Stability and control evaluation of the Pilatus Heli-porter model PC-6/350 airplane
An analysis of the static longitudinal and maneuvering stability and lateral controllability characteristics of the Pilatus "Heli-Porter" Model PC-6/ 350-H-l Airplane was conducted during the months of February, March, and April of 1966. This analysis was conducted at the Forrestal Air...
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| Language: | en_US |
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Princeton University
2012
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| Online Access: | http://hdl.handle.net/10945/9637 |