Experimental Investigation of Aerodynamic Performance of Airfoils Fitted with Morphing Trailing Edges

Contribution for newspaper or weekly magazine English OPEN
Ai, Qing; Kamliya Jawahar, Hasan; Azarpeyvand, Mahdi;
  • Publisher: American Institute of Aeronautics and Astronautics Inc. (AIAA)
  • Identifiers: doi: 10.2514/6.2016-1563
  • Subject:
    acm: ComputingMethodologies_COMPUTERGRAPHICS

The aerodynamic performance and wake development of a NACA 0012 airfoil fitted with morphing trailing edges were studied using experimental and computational techniques. The NACA 0012 airfoil was tested with morphing trailing edges having various camber profiles with th... View more
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