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To Verify Lift Force Generate by 3D Printed Unsymmetrical Airfoil at Zero Angle of Attack

Author(s):

Tahseen Alam , B.I.T SINDRI DHANBAD; Prabhakar, B.I.T SINDRI

Keywords:

NACA Airfoil Solid works, NX Unigraphics, ANSYS

Abstract

Design of aircraft wing is most difficult and its test is very expensive. So very less organization manufacture the aircraft wings. Many researchers try to invent the new wing design which should be simple and test. So for the verification select unsymmetrical airfoil because it will give the lift force even zero angle of attack. Airfoil should be smooth and easy manufacturing for flow simulation use 3d printing technology. Rapid prototype technology provides the ability to fabricate initial prototype from various material. Uses of three analysis software for proper results like compare. All the tree software has advantage like modeling analysis drawing. These solvers compare better and more accurate result.

Other Details

Paper ID: IJSRDV7I30395
Published in: Volume : 7, Issue : 3
Publication Date: 01/06/2019
Page(s): 500-503

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