Throughflow method for turbomachines applicable for all flow regimes

Journal of Turbomachinery

Volumn 119, Issue 2, 1997, Pages 256-262

  Damle, S V ^a   Dang, T Q ^a   Reddy, D R ^b  

^a Syracuse University   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0031512805     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841108     Document Type: Article

References (16)

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11. Marsh, H., 1966, “A Digital Computer Program for the Through-flow Fluid Mechanics in an Arbitrary Turbomachine Using a Matrix Method,” Aeronautical Research Council, R M 3509.
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13. Schmidt, J. F., Royce, M. D., Wood, J. R., and Steinke, R. J., 1987, “Supersonic Through-flow Fan Design,” AIAA Paper No. 87-1746.
14. Smith, L. H., 1966, “The Radial-Equilibrium Equation of Turbomachinery,” ASME Journal of Engineering for Power, Vol. 88, pp. 1-12.
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16. Wu, C. H., 1952, “A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial, Radial and Mixed-Flow Types,” NACA TN 2604.