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Volumn 3 PART A, Issue , 2005, Pages 151-164

Thermal-mechanical life prediction system for anisotropic turbine components

Author keywords

[No Author keywords available]

Indexed keywords

CYCLIC TRANSIENTS; GAS TURBINE ENGINE; MATERIAL PROPERTIES; SHEAR STRAINS;

EID: 27744479822     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2005-68107     Document Type: Conference Paper
Times cited : (10)

References (24)
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    • Arakere, N.J.1
  • 7
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    • Critical plane fatigue modeling and characterization of single crystal nickel superalloys
    • ASME IGTI 2001-GT-30300, April
    • Naik, R.A., DeLuca, D., P., and Shah, D. M., "Critical Plane Fatigue Modeling and Characterization of Single Crystal Nickel Superalloys", ASME IGTI 2001-GT-30300, Journal of Engineering for Gas Turbines and Power, April 2004.
    • (2004) Journal of Engineering for Gas Turbines and Power
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  • 12
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    • Creep Fatigue life prediction for engine hot section materials (isotropic) second annual report
    • March
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    • (1985) NASA CR-174844
    • Moreno, V.1    Nissley, D.M.2    Lin, L.S.3
  • 13
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    • Nissley, D.M.1    Meyer, T.G.2
  • 14
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    • Nov.
    • MacLachlan, D.W., and Knowles, D. M., "The Effect of Material Behavior on the Analysis of Single Crystal Turbine Blades: Part II - Component Analysis", Fatigue Fracture Engineering Material Structures, Vol. 25, pp 399-409, Nov. 2001.
    • (2001) Fatigue Fracture Engineering Material Structures , vol.25 , pp. 399-409
    • MacLachlan, D.W.1    Knowles, D.M.2
  • 15
    • 0347840991 scopus 로고
    • Energy efficient engine high-pressure turbine design report
    • PWA-5594-171, March
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.