Structural and Droptest Analysis of Helicopter Landing Skids | Zendy

D Anitha et al. D Anitha et al. | Zendy

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Structural and Droptest Analysis of Helicopter Landing Skids

Author(s) -

D Anitha et al. D Anitha et al.

Publication year - 2017

Publication title -

international journal of mechanical and production engineering research and development

Language(s) - English

Resource type - Journals

eISSN - 2249-6890

pISSN - 2249-8001

DOI - 10.24247/ijmperdoct201740

Subject(s) - aeronautics , aerospace engineering , landing gear , marine engineering , environmental science , engineering , computer science

Landing skids of Helicopter are directly attached to the helicopter structure. These skids should be able to withstand buckling of struts, stresses &strains. So in the current study, we will consider a Composite material, High strength steel alloy, Aluminum alloy, for the structure and perform structural analysis and drop tests to study which material can perform satisfactorily under normal lending conditions. Helicopter skids are modeled based on the design of an Ultra Light Helicopter.

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