과제정보
본 연구는 국가과학기술연구회에서 지원한 "차세대 항공 모빌리티 안전성 향상 핵심기술연구" 사업 수행 결과의 일부이며, 지원에 감사드립니다.
참고문헌
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- AC 20-107B, Composite aircraft structure, FAA, 2009.
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- AC 25.571, Damage tolerance and fatigue evaluation of structure.
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- Kim, S. J. and Park, S., "Compressive strength prediction of composite laminates containing circular holes," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 49, No. 7, 2021, pp. 549~555. https://doi.org/10.5139/JKSAS.2021.49.7.549