Design and Experiment Study of Coanda Surface at Airfoil Trailing Edge

Author:

Hongyang Liu,Buyuan Hu,Chao Song,Zhu Zhou,Yonggang Yu,Yu Tang

Publisher

Springer Nature Singapore

Reference15 articles.

1. Zou, Y., Yin, Y., Song,.J.: Flight control of a flying-wing UAV based on active disturbance rejection control. In: IEEE 3rd International Conference on Control Science and Systems Engineering (2017)

2. Wang, L., Wang, L.X., Jia, Z.R.: Control allocation method for combat flying wing with multiple control surface[J]. Acta Aeronautica et Astronautica Sinica 32(4), 571–579 (2011)

3. Li, J., Chen, X., Li, Z.: The attitude decoupling control of the flying wing UAV. In: IEEE Chinese Guidance, Navigation and Control Conference (2016)

4. Davidson, I.M.: Aerofoil boundary layer control systems: US3062483A [P] (1962)

5. Abramson, J., Rogers, R.E.: High speed characteristics of circulation control airfoils. In: AIAA 21th Aerospace Science Meeting. Reston: AIAA (1983)

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