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전병희(Byoung-Hee Jeon),양명석(Myoung-Seog Yang),이현승(Hyun-SeungLee),이영신(Young-Shin Lee) 대한기계학회 2008 대한기계학회 춘추학술대회 Vol.2008 No.5
This paper describes the static test results of SmartUAV's Rear-Spar structures. Test sequences are design limit load test, design ultimate load test and design fracture load test. Test results are verified to static strength of SmartUAV's Rear-spar. Rear-spar structures are fractured on 158% design load during design fracture load test.