Numerical Investigation of Stall Characteristics and Stall Control of Circulation Control Airfoil

Author:

Shao Shuai1ORCID,Guo Zheng2,Hou Zhongxi3,Gao Xianzhong4,Jia Gaowei5,Bao Lei6,He Xiangyue7

Affiliation:

1. Test Center, National Univ. of Defense Technology, Xi’an 710106, China. ORCID: .

2. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

3. Professor, Test Center, National Univ. of Defense Technology, Xi’an 710106, China.

4. Associate Professor, Test Center, National Univ. of Defense Technology, Xi’an 710106, China.

5. Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

6. Research Associate, Test Center, National Univ. of Defense Technology, Xi’an 710106, China.

7. Test Center, National Univ. of Defense Technology, Xi’an 710106, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Reference24 articles.

1. Alexander, M. G., S. G. Anders, S. K. Johnson, J. P. Florance, and D. F. Keller. 2005. Trailing edge blowing on a two-dimensional six-percent thick elliptical circulation contro airfoil up to transonic conditions, 1–26. Hampton, VA: NASA Langley Research Center.

2. Englar R. J. G. M. Blaylock R. J. Gaeta G. S. Jones and W. E. Milholen. 2010. “Recent experimental development of circulation control airfoils and pneumatic powered-lift systems.” In Proc. AIAA Paper 2010–345. Reston VA: American Institute of Aeronautics and Astronautics.

3. Design of the Circulation Control Wing STOL Demonstrator Aircraft

4. Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I - Airfoil Development

5. Forster M. 2017. “Computational modelling of transonic circulation control.” Ph.D. thesis School of Engineering Univ. of Liverpool.

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