Preliminary evaluation of thrust loss in commercial aircraft engine due to airborne collision with Unmanned Aerial Vehicles (UAVs)
This paper is devoted to investigating the influence of UAVs airborne collision with civil aircraft engine on the operation safety of commercial aircraft. The damage levels of the civil aircraft fan blades and compressor blades during the UAVs airborne collision are both evaluated based on the Finit...
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Main Authors: | , , , |
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格式: | Conference or Workshop Item |
語言: | English |
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2021
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在線閱讀: | https://hdl.handle.net/10356/148349 |
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