JETIREXPLORE- Search Thousands of research papers



Published in:

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

Unique Identifier

JETIR2006469

Page Number

919-938

Share This Article


Title

Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies

ISSN

2349-5162

Cite This Article

"Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.7, Issue 6, page no.919-938, June-2020, Available :http://www.jetir.org/papers/JETIR2006469.pdf

Abstract

Aircraft has two major components, which are fuselage and wing . An aircraft wing is a most crucial part of any aircraft that produces lift, while moving through air. As such, wings have efficient cross-sections that are subject to aerodynamic forces and act as an airfoils. The aim of this project is to study the deformation caused in the wing of a 2- seater ultra-light aircraft having NACA - 23015 airfoil profile having stringers and without having stringers and to check how much role the stringers can play in reducing the deformation of the wing. The design is done corresponding to the calculated values with the help of designing software Creo 4.0 and the analysis is done to show the structural deformations for the applied loading conditions with the help of ANSYS 19.3, also CFD is done with the help of ANSYS FLUENT (a flow analysis software) to fins the optimum AOA (Angle of Attack)

Key Words

Ultra-light Aircraft, Wing Design Analysis, CAD, CFD, Creo 4.0 Ansys, Lift, Aerodynamics forces, NACA airfoil, Aircraft wing, Design optimization, Finite Element Analysis (FEA)

Cite This Article

"Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 6, page no. pp919-938, June-2020, Available at : http://www.jetir.org/papers/JETIR2006469.pdf

Publication Details

Published Paper ID: JETIR2006469
Registration ID: 234502
Published In: Volume 7 | Issue 6 | Year June-2020
DOI (Digital Object Identifier):
Page No: 919-938
ISSN Number: 2349-5162

Download Paper

Preview Article

Download Paper




Cite This Article

"Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 6, page no. pp919-938, June-2020, Available at : http://www.jetir.org/papers/JETIR2006469.pdf




Preview This Article


Downlaod

Click here for Article Preview