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Volumn 1, Issue , 2005, Pages 209-214

Application of CTOA/CTOD in the residual strength analysis of built-up and integral structures

Author keywords

[No Author keywords available]

Indexed keywords

ADJACENT CRACKS; AIRFRAME STRUCTURAL INTEGRITY; COMMERCIAL TRANSPORT; CRACK PLANE; CRACK TIP OPENING ANGLE; FAILURE SIMULATION; FUSELAGE STRUCTURES; GEOMETRIC NON-LINEAR; INTEGRAL STRUCTURES; LONG LEADS; MULTI-SITE; NASA LANGLEY RESEARCH CENTER; PREDICTION METHODOLOGY; RADIAL PRESSURE; RESIDUAL STRENGTH; SHELL ELEMENT; STIFFENED PANEL; TEST SYSTEMS; THREE-DIMENSIONAL SOLIDS; TOOLSETS; UNIAXIAL TENSIONS;

EID: 84869789115     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (2)

References (11)
  • 1
    • 0002577646 scopus 로고
    • Damage tolerance in pressurized fuselages
    • D. L. Simpson, ed., EMAS Ltd.
    • Swift, T., "Damage Tolerance in Pressurized Fuselages", New Materials and Fatigue Resistant Aircraft Design, D. L. Simpson, ed., EMAS Ltd., 1987, pp. 1-77.
    • (1987) New Materials and Fatigue Resistant Aircraft Design , pp. 1-77
    • Swift, T.1
  • 2
    • 0032021767 scopus 로고    scopus 로고
    • Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure
    • Harris, C. E.; Newman, J. C., Jr.; Piascik, R. and Starnes, J. H., Jr., "Analytical Methodology for Predicting the Onset of Widespread Fatigue Damage in Fuselage Structure", Journal of Aircraft, Vol. 35, No. 2, 1998, pp. 307-317.
    • (1998) Journal of Aircraft , vol.35 , Issue.2 , pp. 307-317
    • Harris, C.E.1    Newman Jr., J.C.2    Piascik, R.3    Starnes Jr., J.H.4
  • 4
    • 0037290881 scopus 로고    scopus 로고
    • Residual strength analyses of stiffened and unstiffened panels - Part I: Laboratory specimens
    • Newman, J. C., Jr., Seshadri, B. R., and Dawicke, D. S., " Residual Strength Analyses of Stiffened and Unstiffened Panels - Part I: Laboratory Specimens," Engineering Fracture Mechanics, 70, 3-4, 2003, pp. 493-508.
    • (2003) Engineering Fracture Mechanics , vol.70 , Issue.3-4 , pp. 493-508
    • Newman Jr., J.C.1    Seshadri, B.R.2    Dawicke, D.S.3
  • 5
    • 0037290691 scopus 로고    scopus 로고
    • Residual strength analyses of stiffened and unstiffened panels - Part II: Wide panels
    • Seshadri, B. R., Newman, J. C., Jr., and Dawicke, D. S., " Residual Strength Analyses of Stiffened and Unstiffened Panels - Part II: Wide Panels," Engineering Fracture Mechanics, 70, 3-4, 2003, pp. 509-524.
    • (2003) Engineering Fracture Mechanics , vol.70 , Issue.3-4 , pp. 509-524
    • Seshadri, B.R.1    Newman Jr., J.C.2    Dawicke, D.S.3
  • 6
    • 0041291802 scopus 로고    scopus 로고
    • Integral airframe structures (IAS) - Validated feasibility study of integrally stiffened metallic fuselage panels for reducing manufacturing costs
    • Munroe, K., Wilkins and Gruber, M., "Integral Airframe Structures (IAS) - Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs," NASA/CR-2000-209337, 2000.
    • (2000) NASA/CR-2000-209337
    • Munroe, K.1    Wilkins2    Gruber, M.3
  • 8
  • 11
    • 0003301950 scopus 로고
    • ZIP3D - An elastic and elastic-plastic finite-element analysis program for cracked bodies
    • Shivakumar, K. N. and Newman, J. C., Jr., "ZIP3D - An Elastic and Elastic-Plastic Finite-Element Analysis Program for Cracked Bodies," NASA TM 102753, 1990.
    • (1990) NASA TM 102753
    • Shivakumar, K.N.1    Newman Jr., J.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.