Composite skid landing gear design investigation
A composite skid landing gear design investigation has been conducted. Limit Drop Test as per Federal Aviation Regulations (FAR) Part 27.725 and Crash test as per MIL STD 1290A (AV) were simulated using ABAQUS to evaluate performance of multiple composite fiber-matrix systems. Load factor developed...
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Georgia Institute of Technology
2008
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| Online Access: | http://hdl.handle.net/1853/24763 |