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Volumn 135, Issue 2, 2012, Pages

A Method to Estimate the Performance Map of a Centrifugal Compressor Stage

Author keywords

[No Author keywords available]

Indexed keywords

ALGEBRAIC EQUATIONS; CENTRIFUGAL COMPRESSOR STAGE; COMPRESSOR IMPELLER; DESIGN POINTS; DIFFERENT SPEED; EMPIRICAL COEFFICIENTS; FLOW COEFFICIENTS; NON-DIMENSIONAL PARAMETERS; PARAMETERIZED EQUATIONS; PERFORMANCE MAPS; PHYSICALLY BASED; PRELIMINARY DESIGN; PRESSURE RATIO; PRIOR KNOWLEDGE; SURGE LINES; VANELESS DIFFUSER;

EID: 84868627154     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.4006590     Document Type: Article
Times cited : (95)

References (13)
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  • 4
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    • Longman Group, Pearson Education Ltd, Harlow, Essex, UK.
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    • (1989) Compressor Aerodynamics
    • Cumpsty, N.A.1
  • 5
    • 84969342707 scopus 로고
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    • 10.1115/1.3677568
    • Rodgers C. Typical Performance Characteristics of Gas Turbine Radial Compressors. ASME J. Eng. Power 1964, 86:161-175. 10.1115/1.3677568
    • (1964) ASME J. Eng. Power , vol.86 , pp. 161-175
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    • (1990) Proceedings of IMechE Conference
    • Swain, E.1
  • 7
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    • Computational Methods for Preliminary Design and Geometry Definition in Turbomachinery
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    • Casey M.V. Computational Methods for Preliminary Design and Geometry Definition in Turbomachinery. 1994, "," AGARD-LS-195, AGARD Lecture Series on Turbomachinery Design using CFD, NASA-Lewis.
    • (1994)
    • Casey, M.V.1
  • 8
    • 0141682766 scopus 로고    scopus 로고
    • Transonic Radial Compressor Inlet Design
    • 10.1243/095765003322315423
    • Lohmberg A. Casey M. Ammann S. Transonic Radial Compressor Inlet Design. Proc. IMechE Part A 2003, 217:367-374. 10.1243/095765003322315423
    • (2003) Proc. IMechE Part A , vol.217 , pp. 367-374
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  • 9
    • 77950646671 scopus 로고    scopus 로고
    • Estimation of the Performance of Turbocharger Compressors at Extremely Low Pressure Ratios
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    • Casey, M.V.1    Schlegel, M.2
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.