Experimental Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3180
Reference10 articles.
1. Performance Enhancement of a Vertical Stabilizer Using Synthetic Jet Actuators: Non-zero Sideslip
2. Obert, E., Aerodynamic Design of Transport Aircraft, IOS Press, Delft, TheNetherlands,2009, pp.413-432.
3. Aerodynamic Design Guidelines of Aircraft Dorsal Fin
4. Effect of Vortex Generators on Transonic Swept Wings
Cited by 3 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
1. Further Investigation of Vertical Stabilizer with Passive Flow Control Devices;AIAA Scitech 2020 Forum;2020-01-05
2. Computational Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin;Journal of Aircraft;2019-09
3. Computational Investigation of Vertical Stabilizer with Vortex Generators and Dorsal Fin;2018 Flow Control Conference;2018-06-24
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