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Volumn 426-432, Issue 3, 2003, Pages 2453-2458

Effects of bond coat processing on the durability of thermal barrier coatings

Author keywords

Durability; Platinum Aluminide Coatings; Processing; Thermal Barrier Coatings

Indexed keywords

DEFORMATION; DEGRADATION; DURABILITY; ELECTRON BEAMS; FRACTURE; PHYSICAL VAPOR DEPOSITION; PLATINUM; SINGLE CRYSTALS; SUPERALLOYS; THERMAL CYCLING; ZIRCONIA;

EID: 0038677467     PISSN: 02555476     EISSN: 16629752     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.426-432.2453     Document Type: Conference Paper
Times cited : (2)

References (11)
  • 1
    • 0002443331 scopus 로고
    • Thermal barrier coatings for aircraft engines - History and directions
    • NASA CP 3312
    • Miller, R. A., "Thermal Barrier Coatings for Aircraft Engines - History and Directions", Thermal Barrier Coating Workshop, NASA CP 3312, p. 17 (1995).
    • (1995) Thermal Barrier Coating Workshop , pp. 17
    • Miller, R.A.1
  • 3
    • 0002443330 scopus 로고
    • Thermal barrier coating experience on GE aircraft engines
    • NASA CP 3312
    • Bose, S. and DeMasi-Marcin, J., "Thermal Barrier Coating Experience on GE Aircraft Engines", Thermal Barrier Coating Workshop, NASA CP 3312, p. 63 (1995).
    • (1995) Thermal Barrier Coating Workshop , pp. 63
    • Bose, S.1    DeMasi-Marcin, J.2
  • 9
    • 0037874304 scopus 로고    scopus 로고
    • Private Communication, UCSB, Jan.
    • Evans, A. G., Private Communication, UCSB, Jan. 2003.
    • (2003)
    • Evans, A.G.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.