Experimental Investigation of Performance of the Rotorcraft Directional Rudder
The paper presents the results of gyrocopter fuselage experiment testing in a wind tunnel. The model subjected to testing was made in 1:8 scale by 3D printing. The tests included the measurement of forces and aerodynamic moments acting on the model, for a variable fuselage sideslip angle (-20º to 20...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
University of Žilina
2024-01-01
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| Series: | Communications |
| Subjects: | |
| Online Access: | https://komunikacie.uniza.sk/artkey/csl-202401-0004_experimental-investigation-of-performance-of-the-rotorcraft-directional-rudder.php |