A New Study on the Gap Effect of an Airfoil with Active Flap Control Based on the Overset Grid Method

Author:

Hu Zhiyuan,Xu Guohua,Shi Yongjie

Funder

Priority Academic Program Development of Jiangsu Higher Education Institutions

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference28 articles.

1. Friedmann PP, Millott TA (1995) Vibration reduction in rotorcraft using active control—a comparison of various approaches. J Guidance, Control, Dynamics 18(4):664–673. https://doi.org/10.2514/3.21445

2. Roth D, Enenkl B, Dieterich O (2006) Active rotor control by flaps for vibration reduction—full scale demonstrator and first flight test results. Paper presented at the 32nd European Rotorcraft Forum, Maastricht, The Netherlands, 2006

3. Straub FK, Kennedy DK, Domzalski DB, Hassan AA, Ngo H, Anand V, Birchette T (2016) Smart material-actuated rotor technology—SMART. J Intell Mater Syst Struct 15(4):249–260. https://doi.org/10.1177/1045389x04042795

4. Straub FK, Anand VR, Birchette TS, Lau BH (2009) SMART rotor development and wind tunnel test. Paper presented at the 35th European Rotorcraft Forum, Hamburg, 2009

5. Gerontakos P, Lee T (2008) PIV study of flow around unsteady airfoil with dynamic trailing-edge flap deflection. Exp Fluids 45(6):955–972. https://doi.org/10.1007/s00348-008-0514-4

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