Modeling and analysis on wing of A380 flight
1Aswani Kodali and 2T.N.Charyulu
1Dept of M.E, Nova college of Engineering &Technology, Jangareddygudem, W.G district;(A.P) 534447, Email: firstname.lastname@example.org
2Dept. of M.E Nova college of Engineering &Technology, Jangareddygudem, W.G district;(A.P) 534447, Email: Tnchoney@gmail.com
We are conducting structural & thermal analysis on AIR BUS A380WING TO Calculate the stress, strain & thermal flux for finding the wing to be safe.
For calculate the stress, strain& flux we have to use software like CATIA for determining model for analysis FEA package ANSYS. For finding the accurate results in ANSYS.CATIA is a surface modeling package, which we can model the wing and we can import it to ANSYS for conducting analysis.
In this analysis we are conducting three different conditions like steady state thermal analysis with uniform pressure &steady state thermal analysis with varying pressure &transient heat analysis on the wing.
By conducting all these three conditions we find out the results and stress, strain& deformation of the wing from the analysis.
Under the above conditions the obtained stress and strain values are within the limiting range. The maximum stresses that wing of a flight can with stand are 700pa. But obtained stress is 400pa. The analyses that are carried on the wing are steady thermal analysis with varying pressure and transient thermal analysis. Under these analyses the wing that was modeled was a safe. The above work can be extended to different parts of flight.
Key words: wing of A380 flight design, modeling, Steady state thermal analysis with uniform pressure, Steady state thermal analysis with varying pressure, Transient thermal Analysis.
International eJournal of Mathematical Sciences, Technology and Humanities
Volume 2, Issue 5, Pages: 885 - 893