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Volumn 12, Issue , 2002, Pages 682-686

An Investigation of the Effects of Reynolds Number on the Performance of 0.6m Impulse Turbines for Different Hub to Tip Ratios

Author keywords

Fixed Guide Vanes; Impulse Turbine; Reynolds Number; Wave Energy

Indexed keywords

FIXED GUIDE VANES; IMPULSE TURBINES;

EID: 1842608383     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (11)

References (6)
  • 1
    • 1842498907 scopus 로고
    • Performance of the Wells Self-rectifying turbine
    • paper number 1368
    • Raghunathan, S., 1985. "Performance of the Wells Self-rectifying turbine". The Aeronautical Journal, paper number 1368.
    • (1985) The Aeronautical Journal
    • Raghunathan, S.1
  • 6
    • 0011755854 scopus 로고    scopus 로고
    • The Concurrent Engineering Approach to the Manufacture of Impulse Turbine Blades using Rapid Prototyping
    • proceedings of the RPA of the Society of Mechanical Engineers, USA, 3rd Quarter
    • Thakker, A., Sheahan, C., Frawley, P. and Khaleeq, H. B., 2001. "The Concurrent Engineering Approach to the Manufacture of Impulse Turbine Blades using Rapid Prototyping". The Rapid Prototyping Journal, proceedings of the RPA of the Society of Mechanical Engineers, USA, 3rd Quarter, vol. 7, No. 3, pp 1-5.
    • (2001) The Rapid Prototyping Journal , vol.7 , Issue.3 , pp. 1-5
    • Thakker, A.1    Sheahan, C.2    Frawley, P.3    Khaleeq, H.B.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.