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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2009.3
- 수록면
- 12 - 16 (5page)
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초록· 키워드
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The laminated sequence and thickness of a composite structure is an important design parameter which affect the strength and impact damage. In this study, it was investigated the residual strength of carbon fiber laminate after impact damage by the experimental investigation. The tensile strength test and compressive strength test were used to find the mechanical properties, previously. Impact test was performed using low-velocity drop-weight test equipment. The impact damages were finally assessed by the compressive strength test. The investigation results revealed the residual strength of the damaged specimens due to the impact damage.
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등록된 정보가 없습니다.
참고문헌 (6)
참고문헌 신청
대한한공 / 2007 / 소형항공기 BASA 시범사업 참여 방안
국토해양부 / 2008 / 소형항공기급 인증기 개발 1차년도 연구결과보고서
ASTM D3039-00 : Tensile Properties of Polymer Matrix Composite Materials
ASTM D6641 : Standard Test Method for Determining the Compressive Properties of Polymer Matrix Composite Laminates Using a Combined Loading Compression (CLC) Test Fixture
ASTM D7136 : Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates
국토해양부 / 2008 / 소형항공기급 인증기 개발 1차년도 연구결과보고서
ASTM D3039-00 : Tensile Properties of Polymer Matrix Composite Materials
ASTM D6641 : Standard Test Method for Determining the Compressive Properties of Polymer Matrix Composite Laminates Using a Combined Loading Compression (CLC) Test Fixture
ASTM D7136 : Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates
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