Computational Analysis Of Incompressible Viscous Flow Over Single And Multi-Element Airfoils

The flow-field around a multi-element airfoil with leading-edge slat and trailing-edge flap in landing configuration was performed as well as the prediction of the time dependent flow over a NACA 0012 airfoil. The two dimensional incompressible Navier-Stokes equations with a numerical method bas...

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Bibliographic Details
Main Author: El-Sayed, Omer Ali
Format: Thesis
Language:English
English
Published: 2003
Online Access:http://psasir.upm.edu.my/id/eprint/12152/1/FK_2003_11.pdf
http://psasir.upm.edu.my/id/eprint/12152/
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Institution: Universiti Putra Malaysia
Language: English
English
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