Books on the topic 'Turbomachinery flow'

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1

Schobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-24675-3.

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2

Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. Berlin, Heidelberg: Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/b137854.

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3

Schobeiri, Meinhard. Turbomachinery flow physics and dynamic performance. 2nd ed. New York: Springer, 2012.

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4

Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. 2nd ed. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

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5

Turbomachinery flow physics and dynamic performance. Berlin: Springer, 2005.

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6

Caughey, D. A. Multigrid calculation of three-dimensional turbomachinery flows. Ithaca, New York: Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.

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7

Montgomery, Matthew D. A three-dimensional linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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8

Lepicovsky, Jan. Use of pressure sensitive paint for diagnostics in turbomachinery flows with shocks. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.

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9

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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10

Chung-hua, Wu. A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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11

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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12

S, Clark William. Prediction of unsteady flows in turbomachinery using the linearized Euler equations on deforming grids. [Washington, DC: National Aeronautics and Space Administration, 1991.

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13

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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14

Steinke, Ronald J. Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage. Cleveland, Ohio: Lewis Research Center, 1989.

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15

Joint, ASCE/ASME Mechanics Conference (1985 Albuquerque N. M. ). Design methods for two-phase flow in turbomachinery: Presented at the ASCE/ASME Mechanics Conference, Albuquerque, New Mexico, June 24-26, 1985. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1985.

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16

Conference, Joint ASCE/ASME Mechanics. Design methods for two-phase flow in turbomachinery: Presented at the ASCE/ASME Mechanics Conference, Albuquerque, New Mexico, June 24-26, 1985. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1985.

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17

Kurkov, Anatole P. Measurement of gust response on a turbine cascade. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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18

Boretti, A. A. Three-dimensional Euler time accurate simulations of fan rotor-stator interactions. Cleveland, Ohio: Lewis Research Centre, 1990.

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19

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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20

Toledo-Velázquez, Miguel, and Fabrizio Fontaneto. Developments in Turbomachinery Flow. Excelic Press LLC, 2018.

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21

Developments in Turbomachinery Flow. Elsevier, 2015. http://dx.doi.org/10.1016/c2014-0-03018-3.

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22

Schobeiri, Meinhard. Turbomachinery Flow Physics and Dynamic Performance. Springer, 2008.

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23

Schobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer London, Limited, 2006.

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24

Schobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer Berlin / Heidelberg, 2010.

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25

Schobeiri, Meinhard T. Turbomachinery Flow Physics and Dynamic Performance. Springer, 2016.

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26

Turbomachinery design and tonal acoustics computations. San Jose, CA: MCAT Institute, 1995.

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27

United States. National Aeronautics and Space Administration., ed. PIV for turbomachinery applications. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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28

Numerical simulation of complex turbomachinery flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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29

B, Lakshminarayana, and NASA Glenn Research Center, eds. Numerical simulation of complex turbomachinery flows. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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30

Max, Platzer, Carta Franklin O, North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel., and North Atlantic Treaty Organization. Advisory Groupfor Aerospace research and Development. Structures and Materials Panel., eds. AGARD manual on aeroelasticity in axial-flow turbomachines. Volume 1: Unsteady turbomachinery aerodynamics. Neuilly sur Seine, France: AGARD, 1987.

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31

ASME. Print Proceedings of the ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition : Volume 2A : Turbomachinery : Axial Flow Fan and Compressor Aerodynamics; Turbomachinery: Unsteady Flows in Turbomachinery. American Society of Mechanical Engineers, The, 2018.

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32

K, Choo Yung, Eiseman Peter R, Reno Charles J, and Lewis Research Center, eds. Interactive grid generation for turbomachinery flow field simulations. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1988.

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33

Montazerin, Nader, Ghasem Akbari, and Moastafa Mahmoodi. Developments in Turbomachinery Flow: Forward Curved Centrifugal Fans. Elsevier Science & Technology, 2015.

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34

Montazerin, Nader, Ghasem Akbari, and Mostafa Mahmoodi. Developments in Turbomachinery Flow: Forward Curved Centrifugal Fans. Elsevier Science & Technology, 2015.

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35

United States. National Aeronautics and Space Administration, ed. Multigrid calculation of three-dimensional turbomachinery flows. Ithaca, New York: Fluid Dynamics and Aerodynamics Program, Sibley School of Mechanical and Aerospace Engineering, Cornell University, 1989.

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36

ASME. Print Proceedings of the ASME Turbo Expo 2018 : Turbomachinery Technical Conference and Exposition : Volume 2B : Turbomachinery : Axial Flow Turbine Aerodynamics; Turbomachinery : Noise, Ducts and Interactions; Turbomachinery: Radial Turbomachinery Aerodynamics. American Society of Mechanical Engineers, The, 2018.

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37

Center, Lewis Research, ed. Validation of viscous and inviscid computational methods for turbomachinery components. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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38

The design/analysis of flows through turbomachinery: A viscous/inviscid approach. [Washington, D.C.]: NASA, 1991.

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39

Center, Lewis Research, and United States. Army Aviation Systems Command., eds. Computer code for predicting coolant flow and heat transfer in turbomachinery. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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40

A, Mulac Richard, Celestina Mark L, and Lewis Research Center, eds. A model for closing the inviscid form of the average-passage equation system. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

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41

Li, Eric L. A parallel multigrid method for predicting compressible flow in turbomachinery. 2004.

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42

United States. National Aeronautics and Space Administration., ed. Current Lewis turbomachinery research: Building on our legacy of excellence. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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43

United States. National Aeronautics and Space Administration., ed. Towards a comprehensive computational simulation system for turbomachinery. [Washington, DC: National Aeronautics and Space Administration, 1994.

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44

1913-, Hawthorne William Sir, and United States. National Aeronautics and Space Administration., eds. Three-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.

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45

Three-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.

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46

Three-dimensional flow in radial turbomachinery and its impact on design. Cambridge, MA: Gas Turbine Laboratory, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1993.

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47

P, Van Hooser Katherine, and United States. National Aeronautics and Space Administration., eds. A general fluid system simulation program to model secondary flows in turbomachinery. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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48

National Aeronautics and Space Administration (NASA) Staff. Three-Dimensional Flow in Radial Turbomachinery and Its Impact on Design. Independently Published, 2019.

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49

United States. National Aeronautics and Space Administration., ed. An interactive grid generation procedure for axial and radial flow turbomachinery. [Washington, DC?]: National Aeronautics and Space Administration, 1990.

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50

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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