Research on wake vortex drag reduction and formation optimization methods for air-based swarm unmanned aerial vehicle
As the high accuracy CFD method is not suitable for the real-time rapid computation of cluster unmanned aerial vehicle（UAV）, a rapid calculation method of equivalent trailing vortex drag reduction is proposed for the rapid optimization of flight formation in the recovery and accompanying phase of sp...
में बचाया:
| मुख्य लेखकों: | , , , , , |
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| स्वरूप: | Artigo |
| भाषा: | Chinês |
| प्रकाशित: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-08-01
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| श्रृंखला: | Hangkong gongcheng jinzhan |
| विषय: | |
| ऑनलाइन पहुंच: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024149 |
| टैग: |
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