Experimental and numerical simulation study of a light UAV impacting a typical airliner flat tail structure
To evaluate the flight safety threat of unmanned aerial vehicle（UAV）to other aircraft in the air，experiments and numerical simulations of UAV impacting the aircraft structure must be carried out. Based on the launch test system of large caliber special-shaped air cannon，the collision experiments bet...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-04-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023201 |
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