COMET 2016

(Conference On Mechanical Engineering & Technology)
in association with
IJSRD – International Journal for Scientific Research & Development
Click here to download Event Brochure

Conference On Mechanical Engineering and Technology (COMET) was commenced with the aim of promoting excellence in the field of mechanical engineering and to provide a platform for bringing out the best among the department’s students. What started as a simple initiative soon spiralled into a conclave. Needless to say it has experienced exponential growth in the sheer number of participants, both internal and external alike, augmented by the quality alongside. The events in its fold have enthused engineers from colleges nationwide thus increasing its domain of influence over the years. Attracting almost 1000 odd external participants in its previous edition, we are confident that these will be more than double positively for the upcoming edition.

COLLOQUIUM

Colloquium,the paper presentation contest, offers a platform to the participants to present & exchange their ideas, innovations and solutions to engineering problems in front of a very scholarly audience. The conference will bring together leading researchers, engineers and scientists in the domain of interest from around the world. COLLOQUIUM is the premier forum for the presentation of new advances and research results in the fields of theoretical and experimental mechanical engineering. Students (B.E/B.Tech./M.Tech./Ph.D.), researchers and qualified personnel interested in the field of mechanical engineering are invited to present papers.

We hope that conference results will lead to significant contributions to the knowledge in these up-to-date engineering and scientific fields.

Topics of interest for submission include, but are not limited to:

Advanced Manufacturing System.
Applications of Aerospace Technology.
Automation and Robotics.
Automobile engineering.
Biomechanics and Bioinstrumentation.
Concurrent Design of Vibration System.
Fluid Mechanics.
Human Values and Professional ethics.
Industrial Management.
Material Science.
Nanotechnology.
Non-Conventional Sources of Energy.
Thermal Engineering

Organized By:

Mechanical Engineering Society,

Mechanical Engineering Department,

IIT(BHU)-Varanasi

Website : http://mesiitbhu.in/comet.html

Publication Partner:

International Journal for Scientific Research & Development
Website : www.ijsrd.com

Design and Linear Static Analysis of Transport Aircraft Vertical Tail for Different Rudder Deflection (Rotation)

#ijsrd journal Recently Published Good Article on Design and Linear Static Analysis of Transport Aircraft Vertical Tail for Different Rudder Deflection (Rotation)

Author(s):

Vinayaka V , AMC Engineering College; Santosh Kumar, AMC Engineering College; Byra Reddy, AMC Engineering College

Keywords:

Static stress analysis, vertical tail, fatigue, AL 7075 T6, CATIA V5 R19, MSC PATRAN and MSC NASTRAN, CFD

Abstract

The design of vertical tail structure varies according to nature of aircraft and its function. The experimental test of vertical tail structure is difficult and more expensive process. In this present work detailed design of transport aircraft vertical tail with rudder structure modelling done by using CATIA V5 R19 software. The static stress analysis is carried out to find the stresses at of the vertical tail with rudder structure for different deflection of rudder. The stresses are estimated to find the safety factor of the structure using finite element approach with the help of MSC/PATRAN and MSC/NASTRAN software. The material used in the vertical tail structure is aluminium 7075-T6, which has high fatigue strength. From the analysis it is found that maximum principal stress of vertical tail structure is less than yield strength of aluminium 7075-T6 alloy. The maximum principal stress value form analysis is used to find fatigue damage calculations for vertical tail structure. The obtained analytical result shows that safe no of fatigue life hours of vertical tail structure. The result is verified with reserve factor approach.

For Full Length Paper visit : http://www.ijsrd.com/Article.php?manuscript=IJSRDV3I100010