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1

Steinke, Ronald J. Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. Cleveland, Ohio: Lewis Research Center, 1986.

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2

Hill, Philip G. An educational introduction to transonic compressor stage design principles. Warrendale, Pa: Society of Automotive Engineers, 1993.

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3

Haynes, Joel M. Active control of rotating stall in a three-stage axial compressor. Cambridge, Mass: Gas Turbine Laboratory, Massachusetts Institute of Technology, 1993.

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4

Wilde, Geoffrey. Flow matching of the stages of axial compressors. Derby: Rolls-Royce Heritage Trust, 1999.

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5

O'Brien, Joseph Morton. Transonic Compressor Test Rig rebuild and initial results with the Sanger stage. Monterey, Calif: Naval Postgraduate School, 2000.

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6

Newman, Frederick A. Experimental vibration damping characteristics of the third-stage rotor of a three-stage transonic axial-flow compressor. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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7

Chmielniak, Tadeusz. SYMKOM'99: International conference compressor & turbine stage flow path theory, experiment & user verification. Łódź: Politechnika Łʹodzka, Instytut Maszn Przeoływowych, 1999.

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8

Swansson, N. S. Investigation of blade vibration T55-L-11C compressor stages 1 and 2. Melbourne, Victoria: Aeronautical Research Laboratories, 1985.

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9

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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10

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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11

Design of 9.271-pressure-ratio five-stage core compressor and overall performance for first three stages. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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12

Analysis of the Sensitivity of Multi-Stage Axial Compressors to Fouling at Various Stages. Storming Media, 2002.

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13

Design of a low aspect ratio transonic compressor stage using CFD techniques. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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14

Simulated dynamic response of a multi-stage compressor with variable molecular weight flow medium. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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15

Center, Langley Research, ed. Simulated dynamic response of a multi-stage compressor with variable molecular weight flow medium. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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16

Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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17

Preliminary Design Code for an Axial Stage Compressor. Storming Media, 2001.

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18

L, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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19

L, Gundy-Burlet Karen, and Ames Research Center, eds. Temporally and spatially resolved flow in a two-stage axial compressor. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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20

Optimizing the Efficiency of a Multi-Stage Axial-Flow Compressor: An Application of Stage-Wise Optimization. Storming Media, 1998.

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21

Transonic Compressor Test Rig Rebuild and Initial Results with the Sanger Stage. Storming Media, 2000.

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22

Dimension determination of precursive stall events in a single stage high speed compressor. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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23

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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24

Facility, Dryden Flight Research, ed. The effect of compressor seventh-stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.

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25

Bayly, Brian. Chemical Change in Deforming Materials. Oxford University Press, 1993. http://dx.doi.org/10.1093/oso/9780195067644.001.0001.

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This book is the first to detail the chemical changes that occur in deforming materials subjected to unequal compressions. While thermodynamics provides, at the macroscopic level, an excellent means of understanding and predicting the behavior of materials in equilibrium and non-equilibrium states, much less is understood about nonhydrostatic stress and interdiffusion at the chemical level. Little is known, for example, about the chemistry of a state resulting from a cylinder of deforming material being more strongly compressed along its length than radially, a state of non-equilibrium that remains no matter how ideal the cylinder's condition in other respects. M. Brian Bayly here provides the outline of a comprehensive approach to gaining a simplified and unified understanding of such phenomena. The author's perspective differs from those commonly found in the technical literature in that he emphasizes two little-used equations that allow for a description and clarification of viscous deformation at the chemical level. Written at a level that will be accessible to many non-specialists, this book requires only a fundamental understanding of elementary mathematics, the nonhydrostatic stress state, and chemical potential. Geochemists, petrologists, structural geologists, and materials scientists will find Chemical Change in Deforming Materials interesting and useful.
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26

Field, John. Therapeutic strategies in managing cardiac arrest. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780199600830.003.0064.

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Emergency and critical care specialists are important interdisciplinary physicians who often impact on the long-term survival of patients sustaining cardiac arrest, as well as immediate outcomes. These specialists are often at the crossroads of survival for patients achieving return of spontaneous circulation, and it is important to appreciate that out-of-hospital and in-hospital cardiac arrest patients represent different pathophysiological subgroups with respect to aetiology and pathophysiology. Important time-dependent triage and therapy are crucial, and efforts to identify and treat pathophysiological triggers share priority with the initiation of hypothermia protocols and other targeted interventions, such as coronary angiography and percutaneous coronary intervention. Updated basic life support (BLS) and advanced life support (ACLS) protocols emphasize the importance of high quality chest compressions as central to achieving return of spontaneous circulation and emphasize that airway interventions should not detract from this objective. No specific ACLS intervention including intubation, vasopressor therapy or use of anti-arrhythmic agents has been found to improve outcome. The goal of both BLS and ACLS protocols is the achievement of return of spontaneous circulation, the prevention of re-arrest and the initiation of immediate post-resuscitation interventions associated with improved outcome. These include targeted temperature management (induced hypothermia) and coronary angiography for appropriate patients and ‘bundled’ critical care for all recognizing that the post-arrest state is a systemic inflammatory condition requiring multidisciplinary care beyond hypothermia and cardiovascular support.
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