The directional stability and control of an airplane during the landing roll
This thesis considers the problem of the directional instability, as exhibited by aircraft with tricycle landing gear, during the landing roll after touchdown. The approximate equations of motion are solved on an analog computer to describe the motion of an aircraft as it moves along the runway afte...
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| Format: | Others |
| Language: | en_US |
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Virginia Polytechnic Institute
2017
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| Online Access: | http://hdl.handle.net/10919/76129 |