Structural and Modal analysis of Air craft wing
ANSYS WORKBENCH14.0,CATIA V5 NUMERICAL MODEL ANALYSIS
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.
"Structural and Modal analysis of Air craft wing", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.3, Issue 11, page no.100 - 109, December-2018, Available :https://ijsdr.org/papers/IJSDR1812017.pdf
Volume 3
Issue 11,
December-2018
Pages : 100 - 109
Paper Reg. ID: IJSDR_180836
Published Paper Id: IJSDR1812017
Downloads: 000347175
Research Area: Engineering
Country: Krishna, Andhra pradesh, India
ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016
An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator
Publisher: IJSDR(IJ Publication) Janvi Wave
