Design and Structural Analysis of Skid Landing Gear

Authors

  • S. Naresh Kumar Mechanical Department, Vardhaman College of Engineering, Shamshabad, India Author
  • J. Abdul Shukur Institute of Aeronautical Engineering, Hyderabad, India Author
  • K. Sriker Mechanical Department, Vardhaman College of Engineering, Shamshabad, India Author
  • A. Lavanya Mechanical Department, Vardhaman College of Engineering, Shamshabad, India Author

Keywords:

The Skid Landing Gear, Composites, Designing, Structural Analysis, landing

Abstract

The undercarriage or landing gear in aviation is the structure that supports an aircraft on the ground and allows it to taxi, takeoff and land. A helicopter is an aircraft that can take off and land vertically also called a rotary aircraft, it can hover and rotate in the air and can move sideways and backwards while aloft. Here the type of landing gear is studied and the designing process is done through CATIA (Computer Aided Three Dimensional Interactive Application). The results from analyzing the stress strain state for the skid landing gear with regards for the physically and geometrically nonlinear scheme of deformation were compared.

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Published

2014-02-28

Issue

Special Issue-2 (Feb 2014)

Section

Articles

How to Cite

Design and Structural Analysis of Skid Landing Gear. (2014). International Journal of Current Engineering and Technology, 1(2.Special Issue), 635-642. https://ijcet.evegenis.org/index.php/ijcet/article/view/3722