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Books on the topic 'Axial turbomachine'

Author: Grafiati
Published: 28 May 2022
Last updated: 31 July 2025

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1

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. AGARD, 1987.

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2

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Blading design for axial turbomachines. AGARD, 1989.

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3

T, Fransson, Sieverding C. H. 1939-, and Von Karman Institute for Fluid Dynamics., eds. Aeroelasticity in axial flow turbomachines: May 3-7, 1999. von Karman Institute for Fluid Dynamics, 1999.

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4

Arasu, A. Valan. Turbo machines. Vikas Publishing House, 2008.

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5

1939-, Sieverding C. H., Hodson H. P, and Von Karman Institute for Fluid Dynamics., eds. Blade row interference effects in axial turbomachinery stages: February 9-12, 1998. Von Karman Institute for Fluid Dynamics, 1998.

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6

United States. National Aeronautics and Space Administration., ed. An interactive grid generation procedure for axial and radial flow turbomachinery. National Aeronautics and Space Administration, 1990.

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7

1945-, Sharma Om P., and United States. National Aeronautics and Space Administration., eds. Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines. National Aeronautics and Space Administration, 1997.

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8

O, Carta F., and North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., eds. AGARD manual on aeroelasticity in axial-flow turbomachines, vol.2. Structural dynamics and aeroelasticity. AGARD, 1988.

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9

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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10

S, Dhadwal Harbans, and NASA Glenn Research Center, eds. Simultaneous optical measurements of axial and tangential steady-state blade deflections. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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11

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. National Aeronautics and Space Administration, 1996.

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12

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. National Aeronautics and Space Administration, 1986.

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13

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

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14

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

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15

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.

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17

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
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18

American Institute of Aeronautics and As. Aeroelasticity in Axial-Flow Turbomachines. AIAA (American Institute of Aeronautics & Ast, 1999.

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19

National Aeronautics and Space Administration. Revised FORTRAN Program for Calculating Velocities and Streamlines on the Hub-Shroud Midchannel Stream Surface of an Axial-, Radial-, or Mixed-Flow Turbomachine or Annular Duct. Programmer's Manual-2. Independently Published, 2022.

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20

Introduction to Axial and Radial Turbomachinery Analysis. Concepts ETI, 1993.

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21

Effects of aerodynamic unsteadiness in axial turbomachines: April 25-29, 2005. Von Karman Institute for Fluid Dynamics, 2005.

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22

Institute, Von KæRmæN. Blade-Row Interference Effects in Axial Turbomachiery Stages (General Publication). Amer Inst of Aeronautics &, 2002.

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23

McCandlish, Felicite Mary. Mathematical and computational aspects of blade row interaction in axial flow turbomachines. 1986.

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24

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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25

Impact of periodic unsteadiness on performance and heat load in axial flow turbomachines. National Aeronautics and Space Administration, 1997.

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26

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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27

Müller, Lasse. Adjoint-Based Optimization of Turbomachinery with Application to Axial and Radial Turbines. von Karman Institute for Fluid Dynamics, 2019. http://dx.doi.org/10.35294/phdt201903.

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28

Proceedings of ASME Turbo Expo 2022 : Turbomachinery Technical Conference and Exposition: Turbomachinery - Axial Flow Fan and Compressor Aerodynamics. American Society of Mechanical Engineers, The, 2022.

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29

Proceedings of ASME Turbo Expo 2022 : Turbomachinery Technical Conference and Exposition: Turbomachinery - Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics. American Society of Mechanical Engineers, The, 2022.

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30

Axial Flow Fans and Compressors: Aerodynamic Design and Performance (Cranfield Series on Turbomachinery Technology). Ashgate Publishing, 1997.

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31

Escudier, Marcel. Introduction to Engineering Fluid Mechanics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.001.0001.

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Turbojet and turbofan engines, rocket motors, road vehicles, aircraft, pumps, compressors, and turbines are examples of machines which require a knowledge of fluid mechanics for their design. The aim of this undergraduate-level textbook is to introduce the physical concepts and conservation laws which underlie the subject of fluid mechanics and show how they can be applied to practical engineering problems. The first ten chapters are concerned with fluid properties, dimensional analysis, the pressure variation in a fluid at rest (hydrostatics) and the associated forces on submerged surfaces, t
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