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Volumn , Issue , 2004, Pages 193-202

R&D program for innovative civil aircraft structures

Author keywords

Civil aircraft structures; Co cured CFRP structures; Light weight structures; Nose structure; Wing structure

Indexed keywords

ALUMINUM ALLOYS; CARBON DIOXIDE; CARBON FIBER REINFORCED PLASTICS; COST EFFECTIVENESS; ENERGY EFFICIENCY; ENGINEERING RESEARCH; FATIGUE OF MATERIALS; PRESSURE EFFECTS; RESIN TRANSFER MOLDING; SANDWICH STRUCTURES;

EID: 7044235882     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (10)
  • 4
    • 7044280515 scopus 로고    scopus 로고
    • Application of a new CFRP sandwich panel to the aircraft nose
    • Hirose, Y. et al., "Application of a New CFRP Sandwich Panel to the Aircraft Nose Structure" Proceedings of the 10th Japan-U.S. Conference on Composite Materials, pp969-977, 2002.
    • (2002) Conference on Composite Materials , pp. 969-977
    • Hirose, Y.1
  • 10
    • 7044243581 scopus 로고    scopus 로고
    • Clarification of mechanical behavior in compression after impact (CAI) and open hole compression (OHC) tests for carbon/polymer composites
    • Ishikawa, T. and Suemasu, H. "Clarification of Mechanical Behavior in Compression After Impact (CAI) and Open Hole Compression (OHC) Tests for Carbon/Polymer Composites" Proceedings of the 10th Japan-U.S. Conference on Composite Materials, pp21-32, 2002.
    • (2002) Proceedings of the 10th Japan-U.S. Conference on Composite Materials , pp. 21-32
    • Ishikawa, T.1    Suemasu, H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.