Handbook of Turbomachinery Second Edition Revised - Ventech!

SL Standard sea-level condition
e Designates the equivalent value in a two-dimensional cascade
i ideal
Superscript
1 Denotes value for a rotor
REFERENCES
1. NASA SP 36 (1965).
2. B. Lakshminarayana, W. R. Britsch, and W. S. Gearhaart, eds., Fluid
Mechanics, Acoustics, and Design of Turbomachinery, Parts I and II, Scientific
and Technical Information Office, NASA, Washington, D.C. (1974).
3. G. K. Serovy, Aerothermodynamics of Aircraft Engine Components (G. C.
Oates, ed.), AIAA Education Series, American Institute of Aeronautics and
Astronautics, Inc., New York (1985).
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5. R. O. Bullock, J. Eng. Power, Trans. ASME, Ser. A, 86: 247–256 (1964).
6. W. G. Steenken, Aerothermodynamics of Aircraft Engine Components (G. C.
Oates, ed.), AIAA Education Series, American Institute of Aeronautics and
Astronautics, Inc., New York (1985).
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8. H. McDonald, Aerothermodynamics of Aircraft Engine Components (G. C.
Oates, ed.), AIAA Education Series, American Institute of Aeronautics and
Astronautics, Inc., New York (1985).
9. R. M. Haleen and J. J. Johnston, ‘‘The Influence of Rotation on Flow in a
Long Rectangular Channel—An Experimental Study,’’ Report M.D. 18,
Mechanical Engineering Dept., Stanford University, Stanford, Calif.
10. J. J. Johnston, ‘‘The Effect of Rotation on Boundary Layers in Turbomachine
Rotors,’’ Report M.D. 24, Mechanical Engineering Dept., Stanford University,
Stanford, Calif.
11. R. C. Dean and Y. S. Senoo, Trans. J. Basic Eng., ASME, Ser. D, Sept.
(1960).
12. ‘‘Secondary Flows in Turbomachines,’’ AGARD Conference Proceedings, no.
469 (1990).
13. L. H. Smith, Jr., Casing Boundary Layers in Multistage Axial Flow
Compressors, Flow Research on Blading, Elsevier, Amsterdam (1969).
14. J. I. Younghans and G. L. Paul, Aircraft Propulsion Technology and Design (G.
C. Oates, ed.), AIAA Education Series, American Institute of Aeronautics and
Astronautics, Inc., New York (1989).
Copyright © 2003 Marcel Dekker, Inc.