Interaction for External Aerodynamics Airfoil Computations with Viscous Interaction
Modeling Viscous Interaction in External Airfoil Aerodynamics
by Rakesh Kumar*, Dr. R. K. P. Yadav,
- Published in Journal of Advances in Science and Technology, E-ISSN: 2230-9659
Volume 3, Issue No. 6, Aug 2012, Pages 1 - 5 (5)
Published by: Ignited Minds Journals
ABSTRACT
Mat FOIL has been developed to model low-speed airfoils quickly and reliably under various airfoils of flow conditions. The method is based on the second order of the viscous vortex possible flow method and the displacement thickness iterative method is right for the viscous effect. The viscous correction is based on an integral formula of two equations, assisted by many empirical correlations and closing relationships. The possibility of simulating the effects of ground proximity is perhaps the most beneficial software module. A mirror image vortices distribution models the influence of the ground effect. The software is used to reliably predict parametric reliance on arbitrary aerodynamic coefficients near the ground. Favorable and unfavorable soil effects that are not at least contingent on the operating height of the airframe above the surface are expected. Interaction for external airfoil aerodynamics with viscous interaction is discussed in this paper.
KEYWORD
Mat FOIL, low-speed airfoils, viscous vortex, displacement thickness, viscous correction, integral formula, mirror image vortices distribution, ground effect, parametric reliance, arbitrary aerodynamic coefficients
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Corresponding Author Rakesh Kumar*
Research Scholar anu906056@gmail.com
