Wing in Ground Effect- 2d Analysis Using Ansys

Abstract

ABSTRACT Wing-in-Ground vehicles and aerodynamically assisted boats take advantage of increased lift and reduced drag of wing sections in the ground proximity. At relatively low speeds or heavy payloads of these craft, a flap at the wing trailing edge can be applied to boost the aerodynamic lift. The influence of a flap on the two-dimensional NACA 4412 airfoil in viscous ground-effect flow is numerically investigated in this study. The computational method consists of a steady-state, incompressible, finite volume method utilizing the K-epsilon turbulence model. Grid generation and solution of the Navier-Stokes equations are completed using computer program Fluent. The code is validated against published experimental and numerical results of unbounded flow with a flap, as well as ground-effect motion without a flap. Aerodynamic forces are calculated, and the effects of Reynolds number and ground height are presented for the airfoil. Changes in the flow introduced with the change in ground height are also discussed. .

Authors and Affiliations

Aananthan M, Aravind VG, Hormese Tharakan, Gouri Shankar Menon

Keywords

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  • EP ID EP395051
  • DOI 10.9790/9622-0808030106.
  • Views 156
  • Downloads 0

How To Cite

Aananthan M, Aravind VG, Hormese Tharakan, Gouri Shankar Menon (2018). Wing in Ground Effect- 2d Analysis Using Ansys. International Journal of engineering Research and Applications, 8(8), 1-6. https://europub.co.uk/articles/-A-395051