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Volumn 5, Issue , 2005, Pages 3515-3530

Analytical predictions and experimental measurements of hydrogen permeability in a microcrack damaged composite

Author keywords

[No Author keywords available]

Indexed keywords

EMPTY WEIGHT; LAUNCH VEHICLES; LEAK PATHS; LEAK RATE;

EID: 28844487939     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (10)
  • 1
    • 16244379933 scopus 로고    scopus 로고
    • Graphite-epoxy primary structure for reusable launch vehicles
    • Huntsville, AL, Sept. 24-26
    • James, W. S., "Graphite-epoxy primary structure for reusable launch vehicles," AIAA, Space Programs and Technologies Conference, Huntsville, AL, Sept. 24-26, 4268, 1996.
    • (1996) AIAA, Space Programs and Technologies Conference , pp. 4268
    • James, W.S.1
  • 8
    • 28844444409 scopus 로고    scopus 로고
    • Prediction of cryogen leak rate through damaged composite laminates
    • submitted to the, January 25
    • Peddiraju, P., Noh, J., Whitcomb, J., and Lagoudas, D.C., "Prediction of Cryogen Leak Rate through Damaged Composite Laminates," submitted to the Journal of Composite Materials, January 25, 2005.
    • (2005) Journal of Composite Materials
    • Peddiraju, P.1    Noh, J.2    Whitcomb, J.3    Lagoudas, D.C.4
  • 10


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.