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Published in:

Volume 7 Issue 6
June-2020
eISSN: 2349-5162

Unique Identifier

JETIR2006250

Page Number

1711-1719

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Title

Review of Wing Rib Design and Analysis of Aircraft

ISSN

2349-5162

Cite This Article

"Review of Wing Rib Design and Analysis of Aircraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.7, Issue 6, page no.1711-1719, June-2020, Available :http://www.jetir.org/papers/JETIR2006250.pdf

Abstract

Ribs are essential component of Aircraft wing. Ribs are used for maintaining aerofoil contour shape of the wing and reduce stress acting on it. The paper focuses determine stress on wing rib with different designs and select the appropriate design. SOLIDWORKS is used for designing and estimating physical properties of design while ANSYS STATIC STRUCTURAL is used for analysis. Conclusion of the wing rib design is done after study of 5 different rib designs.

Key Words

SOLIDWORKS, ANSYS, Contour, stress, wing rib

Cite This Article

"Review of Wing Rib Design and Analysis of Aircraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 6, page no. pp1711-1719, June-2020, Available at : http://www.jetir.org/papers/JETIR2006250.pdf

Publication Details

Published Paper ID: JETIR2006250
Registration ID: 234287
Published In: Volume 7 | Issue 6 | Year June-2020
DOI (Digital Object Identifier):
Page No: 1711-1719
ISSN Number: 2349-5162

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Cite This Article

"Review of Wing Rib Design and Analysis of Aircraft", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 6, page no. pp1711-1719, June-2020, Available at : http://www.jetir.org/papers/JETIR2006250.pdf




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