Development of a dynamic wind tunnel rig for aircraft pure pitching motion
This paper presents the design, fabrication and testing of a dynamic wind tunnel test rig that is used in conjunction with aircraft dynamics theory in estimating aerodynamics stability derivatives. The value of and can be obtained from free oscillation theory of pure pitching motion. The rig compris...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Faculty of Mechanical Engineering,
2000-12.
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| Subjects: | |
| Online Access: | Get fulltext |