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Volumn 1, Issue , 2007, Pages 19-28

Advanced capabilities for gas turbine engine performance simulations

Author keywords

Distributed computing; Simulation; Web services; Zooming

Indexed keywords

COMPONENT ZOOMING; COMPRESSOR STAGE STACKING METHOD; ZOOMING;

EID: 34548807099     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2007-27086     Document Type: Conference Paper
Times cited : (24)

References (30)
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  • 2
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  • 3
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  • 8
    • 84885267009 scopus 로고    scopus 로고
    • SAE AS681-H, Gas Turbine Engine Steady State and Transient Performance Presentation for Digital Computer Programs.
    • SAE AS681-H, "Gas Turbine Engine Steady State and Transient Performance Presentation for Digital Computer Programs".
  • 9
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  • 10
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  • 18
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    • Design and Development of a 12:1 Pressure Ratio Compressor for the Ruston 6-MW Gas Turbine
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  • 23
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.