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Volumn , Issue , 2005, Pages 39-48

Application of a real-fluid turbomachinery analysis to rocket turbopump geometries

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBLE FLOW; IMPELLERS; INCOMPRESSIBLE FLOW; PUMPS; ROCKET ENGINES;

EID: 30744434427     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1007     Document Type: Conference Paper
Times cited : (3)

References (18)
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    • October
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    • Thin layer approximation and algebraic model for separated turbulent flow
    • Huntsville, AL, January
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  • 11
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    • Sandia Corporation, Livermore, CA, Private Communication, December
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.