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Volumn , Issue , 1996, Pages 322-330

Failure mechanisms around the interface between a sandwich skin and a bonded frame

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MANUFACTURE; AIRFRAMES; STRUCTURAL DYNAMICS; ADHESIVES; FAILURE (MECHANICAL); FINITE ELEMENT METHOD; FORECASTING; INTERFACES (MATERIALS); LOADS (FORCES); MATHEMATICAL MODELS; MECHANICAL TESTING; SANDWICH STRUCTURES; STRENGTH OF MATERIALS; STRESS ANALYSIS; STRUCTURAL FRAMES;

EID: 0029706509     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1353     Document Type: Conference Paper
Times cited : (1)

References (6)
  • 4
    • 0003296653 scopus 로고
    • Development of a Structural Test Simulating Pressure Pillowing Effects in a Bonded Skin/Stringer/Frame Configuration
    • Salt Lake City, UT, June
    • Minguet, P.J., et al., “Development of a Structural Test Simulating Pressure Pillowing Effects in a Bonded Skin/Stringer/Frame Configuration,” Proceedings of the Fourth NASA/DoD Advanced Composite Technology Conference, Salt Lake City, UT, June 1993.
    • (1993) Proceedings of the Fourth Nasa/Dod Advanced Composite Technology Conference
    • Minguet, P.J.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.