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Experimental and Numerical Analysis of Repairing a Triangular Shaped Airfoil

[+] Author Affiliations
F. Etemadi, M. Mani

Amirkabir University of Technology, Tehran, Tehran, Iran

M. Etemadi

Islamic Azad University, Langroud Branch, Guilan, Iran

Paper No. AJK2011-15022, pp. 3455-3461; 7 pages
doi:10.1115/AJK2011-15022
From:
  • ASME-JSME-KSME 2011 Joint Fluids Engineering Conference
  • ASME-JSME-KSME 2011 Joint Fluids Engineering Conference: Volume 1, Symposia – Parts A, B, C, and D
  • Hamamatsu, Japan, July 24–29, 2011
  • Conference Sponsors: Fluids Engineering Division
  • ISBN: 978-0-7918-4440-3
  • Copyright © 2011 by ASME

abstract

This article investigates the aerodynamic characteristics of repairing the airfoil with triangular damage by the measurement of aerodynamic coefficients improvement. For study of this model “two applied and numerical methods are used”. A full span NACA 641 -412 airfoil is considered as test model. Using model is in five schematics: undamaged model, damaged model with upper, lower and full repair model. The used repair sheets are chosen based on the ABDR manuals. Effect of the repair on different shape of damage has performed by the quantity and quality results.

Copyright © 2011 by ASME

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