Numerical Study of Transient Behavior of a NACA 0008 Airfoil Equipped with a Gurney Flap Using a Control-Volume Based Finite-Element Collocated Scheme

Mahzad Khoshlessan, Seyed Mohammad Hossein Karimian, Mahmoud Mani
  • January 2014, American Institute of Aeronautics and Astronautics (AIAA)
  • DOI: 10.2514/6.2014-1109

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http://dx.doi.org/10.2514/6.2014-1109

The following have contributed to this page: Professor Mahmoud Mani and mahzad khoshlessan