| Full Scale Airframe Static Test of 4 Seater Canard Airplane |
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Jeong-Woo Shin, Sung-Chan Kim, Sung-Jun Kim, Dong-Chul Chae, Sang-Wook Lee, Tae-Uk Kim, Jae-Yeul Shim |
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KARI |
| 4인승 선미익 경항공기 전기체 정적 구조시험 |
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신정우, 김성찬, 김성준, 채동철, 이상욱, 김태욱, 심재열 |
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한국항공우주연구원 |
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| Abstract |
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In this paper, full-scale airframe static test of 4-seater canard airplane(the Firefly) was explained. From the results of the structural analysis, 5 design limit loads test conditions and 11 design ultimate loads test conditions were selected. Test loads analysis was performed and test fixtures and load control system(LCS) were prepared to realize the test loads. To protect the test article during the test, the overload protection system was prepared. Strain and deflection values were acquired through the data acquisition system(DAS) to verify the structural analysis results. |
| Key Words:
Full-Scale Static Test, Canard Airplane, Design Limit Loads, Design Ultimate Loads, Test Loads, Overload Protection System |
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