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...
محفوظ في:
| المؤلفون الرئيسيون: | , , , , , |
|---|---|
| التنسيق: | Artigo |
| اللغة: | Chinês |
| منشور في: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-08-01
|
| سلاسل: | Hangkong gongcheng jinzhan |
| الموضوعات: | |
| الوصول للمادة أونلاين: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024149 |
| الوسوم: |
لا توجد وسوم, كن أول من يضع وسما على هذه التسجيلة!
|