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Volumn 51, Issue 4, 2001, Pages 345-359

Numerical investigation of a crash test of a composite helicopter subfloor structure

Author keywords

Aircraft; Composite materials; Crashworthiness; Finite element analysis; Helicopter

Indexed keywords

AIRCRAFT MATERIALS; COMPUTER SIMULATION; CRASHWORTHINESS; ENERGY ABSORPTION; FINITE ELEMENT METHOD; HELICOPTERS;

EID: 0035308326     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00150-1     Document Type: Article
Times cited : (84)

References (17)
  • 2
    • 0005000111 scopus 로고
    • Military standard: Light fixed wing and rotary wing aircraft crash resistance MIL-STD-1290 A (AV) September
    • (1988)
  • 6
    • 0005091266 scopus 로고
    • IMT-2002 Crashworthiness for Commercial AircraftEU RTD Project
    • (1993)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.