Journal of the Korean Society for Aviation and Aeronautics (한국항공운항학회지)
- Volume 13 Issue 3
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- Pages.97-109
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- 2005
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- 1225-9705(pISSN)
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- 2466-1791(eISSN)
Canard Type Aircraft Structural Test
선미익형 항공기 구조시험
- Published : 2005.09.30
Abstract
A canard type aircraft, which has good wing stall and stall/spin-proof characteristics, is under development. The aircraft prototype has full-depth core sandwich type wing and fixed landing gear, and has been built for test flights. Newly developing aircraft will be equipped with retractable landing gear and conventional foam core sandwich laminate structures and multi-rib wings. In this study, we present the structural test procedure and result for aircraft Firefly.
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