Author:
Shao Shuai,Jia Gaowei,Yin Peng,Hou Zhongxi,Zhang Laiping,Guo Zheng
Funder
National Natural Science Foundation of China
Science and Technology Program of Hunan Province
Reference54 articles.
1. Effect of trailing edge flap deflection on bi-static radar cross section of a wing;Nath Dubba,2021
2. NATO AVT-239 Task Group: ‘Innovative Control Effectors for Manoeuvring of Air Vehicles’ – Introduction and overview;Smith,2019
3. Unsteady fluidic oscillators for active controlling boundary layer separation in an ultra-high-lift low-pressure turbine;Qu;Aerosp. Sci. Technol.,2021
4. Analytical study on the synthetic jet control of asymmetric flow field of flying wing unmanned aerial vehicle;Xu;Aerosp. Sci. Technol.,2016
5. Comparison of different plasma actuation strategies for aeroelastic control on a linear compressor cascade;De Giorgi;Aerosp. Sci. Technol.,2021
Cited by
5 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献