INTERNATIONAL JOURNAL OF SCIENTIFIC DEVELOPMENT AND RESEARCH International Peer Reviewed & Refereed Journals, Open Access Journal ISSN Approved Journal No: 2455-2631 | Impact factor: 8.15 | ESTD Year: 2016
open access , Peer-reviewed, and Refereed Journals, Impact factor 8.15
This paper presents modal analysis of aircraft wing. Aircraft wing used for investigation is A300 (wing structure consist of NACA64A215). A cad model of a aircraft wing has been developed using modeling software CATIA V5 and modal analysis was carried out by using ANSYS WORKBENCH14.0.modal analysis has been carried out by fixing one end ( root chord) of aircraft wing while other end( tip chord) is free. The interest is to find the 6 modes of vibration with its respective natural frequency and mode shapes. To validate a project experimental modal analysis of cantilever beam was performed. The result of EMA was compared with numerical modal analysis as well as analytical frequency of cantilever beam. This paper only represent numerical modal analysis of aircraft wing and is validated by considering aircraft wing as a cantilever beam.
Keywords:
ANSYS WORKBENCH14.0,CATIA V5 NUMERICAL MODEL ANALYSIS
Cite Article:
"Structural and Modal analysis of Air craft wing", International Journal of Science & Engineering Development Research (www.ijsdr.org), ISSN:2455-2631, Vol.3, Issue 11, page no.100 - 109, December-2018, Available :http://www.ijsdr.org/papers/IJSDR1812017.pdf
Downloads:
000337074
Publication Details:
Published Paper ID: IJSDR1812017
Registration ID:180836
Published In: Volume 3 Issue 11, December-2018
DOI (Digital Object Identifier):
Page No: 100 - 109
Publisher: IJSDR | www.ijsdr.org
ISSN Number: 2455-2631
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