메뉴 건너뛰기




Volumn 5, Issue , 2005, Pages 135-144

Development of parametric mass and volume models for an aerospace SOFC/gas turbine hybrid system

Author keywords

Auxiliary Power Unit; Hybrid Gas Turbine System; Solid Oxide Fuel Cell (SOFC)

Indexed keywords

AEROSPACE POWER SYSTEMS; AUXILIARY POWER UNIT; COMPONENT SIZING; HYBRID GAS TURBINE SYSTEM;

EID: 27744551801     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2005-68334     Document Type: Conference Paper
Times cited : (43)

References (11)
  • 2
    • 84885320273 scopus 로고    scopus 로고
    • Hybrid solid oxide fuel cell/ gas turbine technology for auxiliary aerospace power
    • Abstract Submitted Reno, NV
    • Steffen, C.J. Jr., Freeh, J.E., Larosiliere, L.M., "Hybrid Solid Oxide Fuel Cell/ Gas Turbine technology for Auxiliary Aerospace Power", Abstract Submitted to ASME IGTI Conference, Reno, NV (2005).
    • (2005) ASME IGTI Conference
    • Steffen Jr., C.J.1    Freeh, J.E.2    Larosiliere, L.M.3
  • 11
    • 0004251733 scopus 로고    scopus 로고
    • Taylor and Francis, Ann Arbor, Michigan
    • nd Edition, Taylor and Francis, Ann Arbor, Michigan.
    • (1999) nd Edition
    • Lefebvre, A.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.