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Volumn , Issue , 2000, Pages

High temperature performance evaluation of a compliant foil seal

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; DYNAMIC LOADS; FOIL BEARINGS; LEAKAGE (FLUID); NASA; SIMULATORS; SOLID LUBRICANTS;

EID: 0012168111     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (13)

References (8)
  • 3
    • 53449096118 scopus 로고
    • A Feasibility Study on the Use of Foil Bearings in Cryogenic T u r b o p u m p s
    • June 24-26, Sacramento, CA, Paper No. AIAA-91-2103
    • Heshmat, H., 1991, "A Feasibility Study on the Use of Foil Bearings in Cryogenic T u r b o p u m p s. " p r e s e n t e d at AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference, June 24-26, Sacramento, CA, Paper No. AIAA-91-2103.
    • (1991) AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference
    • Heshmat, H.1
  • 4
    • 0000697321 scopus 로고
    • Compliant Foil Bearing Structural Stiffness Analysis Part I: Theoretical Model Including Strip and Variable Bump Foil Geometry
    • Ku, C.-P.R., and Heshmat, H.,1992, "Compliant Foil Bearing Structural Stiffness Analysis Part I: Theoretical Model Including Strip and Variable Bump Foil Geometry," Journal of Tribology, Tram. ASME Vol. 113, no. 2,pp. 364-369.
    • (1992) Journal of Tribology, Tram. ASME , vol.113 , Issue.2 , pp. 364-369
    • Ku, C.-P.R.1    Heshmat, H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.