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Books on the topic 'Axial flow impeller blades'

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Author: Grafiati
Published: 4 June 2021
Last updated: 20 February 2023

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1

Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: Von Karman Institute, 1985.

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2

Neuhoff, F. Modifications to the inlet flow field of a transonic compressor rotor. Monterey, Calif: Naval Postgraduate School, 1985.

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3

Arasu, A. Valan. Turbo machines. New Delhi: Vikas Publishing House, 2008.

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4

Wasserbauer, Charles A. NASA low-speed axial compressor for fundamental research. Cleveland, Ohio: Lewis Research Center, 1995.

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5

Escudier, Marcel. Flow through axial-flow-turbomachinery blading. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0014.

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This chapter is concerned primarily with the flow of a compressible fluid through stationary and moving blading, for the most part using the analysis introduced in Chapter 11. The principles of dimensional analysis are applied to determine the appropriate non-dimensional parameters to characterise the performance of a turbomachine. The analysis of incompressible flow through a linear cascade of aerofoil-like blades is followed by the analysis of compressible flow. Velocity triangles for flow relative to blades, and Euler’s turbomachinery equation, are introduced to analyse flow through a rotor. The concepts introduced are applied to the analysis of an axial-turbomachine stage comprising a stator and a rotor, which applies to either a compressor or a turbine.
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6

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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7

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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8

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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9

NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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10

NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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11

NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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12

F, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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13

United States. National Aeronautics and Space Administration. and United States. Army Aviation Systems Command., eds. Unsteady flows in a single-stage transonic axial-flow fan stator row. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

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14

1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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15

Ya, Timofeev I., Shipilov S. D, and United States. National Aeronautics and Space Administration., eds. Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories. Washington, DC: National Aeronautics and Space Administration, 1988.

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16

D, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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17

D, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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