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Volumn , Issue , 2009, Pages

Analysis of turbofan design options for an advanced single-aisle transport aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT GAS TURBINE ENGINES; AIRCRAFT SYSTEMS; DESIGN TRADES; ENABLING TECHNOLOGIES; ENGINE EFFICIENCY; FUEL EFFICIENCY; FUTURE DESIGNS; HIGH BYPASS RATIO; LOWER NOISE; PROPULSION SYSTEM; SIZE CLASS; SPECIFIC FUEL CONSUMPTION; TURBOFAN DESIGN; ULTRA-HIGH;

EID: 78249254271     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (18)

References (27)
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  • 10
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    • Onat, E.1    Klees, G.2
  • 12
    • 69949161657 scopus 로고    scopus 로고
    • An object-oriented computer code for aircraft engine weight estimation
    • June 9-13
    • Tong, M.T., Naylor, B.A., "An Object-Oriented Computer Code for Aircraft Engine Weight Estimation," GT2008-50062, ASME Turbo-Expo 2008, June 9-13, 2008.
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    • Tong, M.T.1    Naylor, B.A.2
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  • 18
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    • Stone, J.R., Krejsa, E.A., Clark, B.J., and Berton, J.J., "Jet Noise Modeling for Suppressed and Unsuppressed Aircraft in Simulated Flight," NASA TM-2009-215524, 2009.
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    • Stone, J.R.1    Krejsa, E.A.2    Clark, B.J.3    Berton, J.J.4
  • 22
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    • AST critical propulsion and noise reduction technologies for future commercial subsonic engines - Separate-flow exhaust system noise reduction evaluation
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.