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Experimental and numerical investigation of flutter phenomenon of an aitcraft wing (NACA 0012)

(2017) MECHANIKA. 23(4). p.562-566
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Abstract
Floating is a dangerous phenomenon for aircrafts and usually ends with plane rupture. It can be used to characterize a dynamic instability of the structure. Floating phenomenon is usually due to an interaction between aerodynamics, elasticity and inertial forces. It appears at a determinate speed of flight called critical floating speed. The aim of the present study is to determine the floating critical speed of an aircraft wing in a subsonic fan by means of experimental tests and numerical simulations using the commercial Finite Element Analysis package ANSYS CFX. The obtained experimental results are in good agreement with those obtained using the numerical approach.
Keywords
Aerodynamics, Floating, Flutter phenomenon, Aircraft wing, Finite Element Analysis, Computational Fluid Dynamics

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MLA
Khatir, Tawfiq, et al. “Experimental and Numerical Investigation of Flutter Phenomenon of an Aitcraft Wing (NACA 0012).” MECHANIKA, vol. 23, no. 4, 2017, pp. 562–66, doi:10.5755/j01.mech.23.4.15175.
APA
Khatir, T., Djillali, B., Khatir, S., Abdelkader, L., & Abdel Wahab, M. (2017). Experimental and numerical investigation of flutter phenomenon of an aitcraft wing (NACA 0012). MECHANIKA, 23(4), 562–566. https://doi.org/10.5755/j01.mech.23.4.15175
Chicago author-date
Khatir, Tawfiq, Boutchicha Djillali, Samir Khatir, Lousdad Abdelkader, and Magd Abdel Wahab. 2017. “Experimental and Numerical Investigation of Flutter Phenomenon of an Aitcraft Wing (NACA 0012).” MECHANIKA 23 (4): 562–66. https://doi.org/10.5755/j01.mech.23.4.15175.
Chicago author-date (all authors)
Khatir, Tawfiq, Boutchicha Djillali, Samir Khatir, Lousdad Abdelkader, and Magd Abdel Wahab. 2017. “Experimental and Numerical Investigation of Flutter Phenomenon of an Aitcraft Wing (NACA 0012).” MECHANIKA 23 (4): 562–566. doi:10.5755/j01.mech.23.4.15175.
Vancouver
1.
Khatir T, Djillali B, Khatir S, Abdelkader L, Abdel Wahab M. Experimental and numerical investigation of flutter phenomenon of an aitcraft wing (NACA 0012). MECHANIKA. 2017;23(4):562–6.
IEEE
[1]
T. Khatir, B. Djillali, S. Khatir, L. Abdelkader, and M. Abdel Wahab, “Experimental and numerical investigation of flutter phenomenon of an aitcraft wing (NACA 0012),” MECHANIKA, vol. 23, no. 4, pp. 562–566, 2017.
@article{8530979,
  abstract     = {{Floating is a dangerous phenomenon for aircrafts and usually ends with plane rupture. It can be used to characterize a dynamic instability of the structure. Floating phenomenon is usually due to an interaction between aerodynamics, elasticity and inertial forces. It appears at a determinate speed of flight called critical floating speed. The aim of the present study is to determine the floating critical speed of an aircraft wing in a subsonic fan by means of experimental tests and numerical simulations using the commercial Finite Element Analysis package ANSYS CFX. The obtained experimental results are in good agreement with those obtained using the numerical approach.}},
  author       = {{Khatir, Tawfiq and Djillali, Boutchicha and Khatir, Samir and Abdelkader, Lousdad and Abdel Wahab, Magd}},
  issn         = {{1392-1207}},
  journal      = {{MECHANIKA}},
  keywords     = {{Aerodynamics,Floating,Flutter phenomenon,Aircraft wing,Finite Element Analysis,Computational Fluid Dynamics}},
  language     = {{eng}},
  number       = {{4}},
  pages        = {{562--566}},
  title        = {{Experimental and numerical investigation of flutter phenomenon of an aitcraft wing (NACA 0012)}},
  url          = {{http://doi.org/10.5755/j01.mech.23.4.15175}},
  volume       = {{23}},
  year         = {{2017}},
}

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