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DESIGN AND FINITE ELEMENT ANALYSIS OF AIRCRAFT …

International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 04 Issue: 06 | June -2017 p-ISSN: 2395-0072 2017, IRJET | Impact Factor value: | ISO 9001:2008 Certified Journal | Page 2133 DESIGN AND FINITE ELEMENT ANALYSIS OF AIRCRAFT WING USING RIBS AND SPARS Sivarama Prasad Peruru 1 , Suman Babu Abbisetti 2 , student, mechanical enginnering Aditya Engineering College, Surampalem 2 Assistant professor,mechanical enginnering, Aditya Engineering College, Surampalem ---------------------------------------- --------------------------------**------ ---------------------------------------- -------------------------ABSTRACT - In this thesis, project detailed DESIGN of tr

Finite element method being a flexible tool is used in various industries to solve several practical engineering problems. In nite element method it is feasible to generate the relative results. V. RESULTS AND DISCUSSIONS: Models of aircraft wing using ribs and spars done in pro-e Fig4: wing ribs and spars

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