Volume : IV, Issue : VIII, August - 2015

Design and Analysis of A General Aviation Aircraft Wing Structure

M. Sampath Kumar Reddy, G. Parthasarathy, G. Sri Bhavya

Abstract :

In the present study, design analysis is performed to accurately estimate the gross take–off weight, define the external geometry, and size the wings of a general aviation aircraft by using the performance parameters associated with a pre–defined mission profile and a set of design goals. Three–dimensional layout and projections of the design airplane are created using CATIA. In addition, finite element software package ANSYS is implemented to perform static stress analysis on the selected wing configuration when subjected to the generated aerodynamic loads to examine its structural reliability. The finite element results have shown that the selected wing configuration is a safe candidate for the present general aviation airplane implementation.

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Article: Download PDF   DOI : 10.36106/ijsr  

Cite This Article:

M. Sampath Kumar Reddy, G. Parthasarathy, G.Sri Bhavya Design and Analysis of A General Aviation Aircraft Wing Structure International Journal of Scientific Research, Vol : 4, Issue : 8 August 2015

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