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Книги з теми "Turbine engines materials"

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Автор: Grafiati
Опубліковано: 6 вересня 2023

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1

E, Helms Harold, ed. Ceramic applications in turbine engines. Park Ridge, N.J., U.S.A: Noyes Publications, 1986.

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2

The Impact of advanced materials on small turbine engines. [Warrendale, Pa: Society of Automotive Engineers, 1991.

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3

P, Millan P., and United States. National Aeronautics and Space Administration., eds. Oxide-dispersion-strengthened turbine blades: Materials for advanced turbine engines, project completion report, project 4. [Phoenix, Ariz.]: Garrett Turbine Engine Co., 1987.

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4

P, Millan P., and United States. National Aeronautics and Space Administration., eds. Oxide-dispersion-strengthened turbine blades: Materials for advanced turbine engines, project completion report, project 4. [Phoenix, Ariz.]: Garrett Turbine Engine Co., 1987.

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5

Wallace, William. Methods for crack growth testing in gas turbine engine disc materials. Ottawa: National Aeronautical Establishment, 1987.

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6

Miller, Robert A. Thermal barrier coatings for gas turbine and diesel engines. [Washington, D.C.]: NASA, 1990.

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7

J, Brindley W., Bailey M. Murray, and United States. National Aeronautics and Space Administration., eds. Thermal barrier coatings for gas turbine and diesel engines. [Washington, D.C.]: NASA, 1990.

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8

Melvin, Freling, Friedrich L. A, and Lewis Research Center, eds. Materials for Advanced Turbine Engines (MATE): Project 4--erosion resistant compressor airfoil coating. [Cleveland, Ohio]: National Aeronautics and Space Administration, 1987.

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9

M, Baldwin Richard, Schick Wilbur R, United States. National Aeronautics and Space Administration., and United States. Army Aviation Systems Command., eds. Spray automated balancing of rotors: Methods and materials. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

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10

Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Turbine engine hot section technology 1986: Proceedings of a conference. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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11

United States. National Aeronautics and Space Administration., ed. Durability testing of commercial ceramic materials: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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12

United States. National Aeronautics and Space Administration., ed. Durability testing of commercial ceramic materials: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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13

Bose, S. Materials for advanced turbine engines (MATE) project 3 design, fabrication and evaluation of an oxide dispersion strengthened sheet alloy combustor liner. [Washington, DC: National Aeronautics and Space Administration, 1990.

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14

David, Nathenson, Prakash Vikas, and NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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15

David, Nathenson, Prakash Vikas, and NASA Glenn Research Center, eds. Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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16

Stephens, Joseph R. Intermetallic and ceramic matrix composites for 815 to 1370 C (1500 to 2500 F) gas turbine engine applications. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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17

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting. Damage tolerance concepts for critical engine components: Papers presented at the 60th Meeting of the Structures and Materials Panel in San Antonio, Texas, USA on 22-26 April 1985. Neuilly sur Seine, France: AGARD, 1985.

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18

ASME International Gas Turbine and Aeroengine Congress and Exposition (33rd 1988 Amsterdam, Netherlands). Toward improved durability in advanced aircraft engine hot sections: Presented at the 1988 ASME Turbo Expo - Land, Sea & Air, the 33rd ASME International Gas Turbine and Aeroengine Congress and Exposition, Amsterdam, the Netherlands, June 5-9, 1988 : sponsored by the Aircraft Committee, ASME International Gas Turbine Institute. New York: American Society of Mechanical Engineers, 1988.

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19

Analysis of an advanced technology subsonic turbofan incorporating revolutionary materials. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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20

Nonlinear control of a reusable rocket engine for life extension. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

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21

Durability testing of commercial ceramic materials: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1996.

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22

Evaluation of PS 212 coatings under boundary lubrication conditions with an ester-based oil to 300⁰C. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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23

Modeling of high-strain-rate deformation, fracture, and impact behavior of advanced gas turbine engine materials at low and elevated temperatures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

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24

Kollmann, Karl, Calum E. Douglas, and S. Can Gülen. Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students. ASME, 2021. http://dx.doi.org/10.1115/1.884676.

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Анотація:
This book is a unique blend of history, technology review, theoretical fundamentals, and design guide. The subject matter is primarily piston aeroengine superchargers – developed in Germany during the Second World War (WWII) – which are centrifugal compressors driven either by the main engine crankshaft or by an exhaust gas turbine. The core of the book is an unpublished manuscript by Karl Kollmann, who was a prominent engineer at Daimler-Benz before and during the war. Dr. Kollmann’s manuscript was discovered by Calum Douglas during his extensive research for his earlier book on piston aeroengine development in WWII. It contains a wealth of information on aerothermodynamic and mechanical design of centrifugal compressors in the form of formulae, charts, pictures, and rules of thumb, which, even 75 years later, constitute a valuable resource for engineering professionals and students. In addition to the translation of the original manuscript from German, the authors have completely overhauled the chapters on the aerothermodynamics of centrifugal compressors so that the idiosyncratic coverage (characteristic of German scientific literature at that time) is familiar to a modern reader. Furthermore, the authors added chapters on exhaust gas turbines (for turbo-superchargers), piston aeroengines utilizing them, and turbojet gas turbines. Drawing upon previously unpublished material from the archived German documents, those chapters provide a concise but technically precise and informative look into those technologies, where great strides were made in Germany during the war. In summary, the coverage is intended to be useful not only to history buffs with a technical bent but also to the practicing engineers and engineering students to help with their day-to-day activities in this particular field of turbomachinery.
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25

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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Анотація:
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, the relationship between pressure and velocity in the absence of viscosity, and fluid flow through straight pipes and bends. The examples used to illustrate the application of this introductory material include the calculation of rocket-motor thrust, jet-engine thrust, the reaction force required to restrain a pipe bend or junction, and the power generated by a hydraulic turbine. Compressible-gas flow is then dealt with, including flow through nozzles, normal and oblique shock waves, centred expansion fans, pipe flow with friction or wall heating, and flow through axial-flow turbomachinery blading. The fundamental Navier-Stokes equations are then derived from first principles, and examples given of their application to pipe and channel flows and to boundary layers. The final chapter is concerned with turbulent flow. Throughout the book the importance of dimensions and dimensional analysis is stressed. A historical perspective is provided by an appendix which gives brief biographical information about those engineers and scientists whose names are associated with key developments in fluid mechanics.
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26

Elevated temperature biaxial fatigue. [Washington, DC]: National Aeronautics and Space Administration, 1985.

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27

Panigrahi, Shashi Kanta, and Niranjan Sarangi. Aero Engine Combustor Casing. Taylor & Francis Group, 2020.

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28

Sarangi, Niranjan, and Sashi Kanta Panigrahi. Aero Engine Combustor Casing: Experimental Design and Fatigue Studies. Taylor & Francis Group, 2017.

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29

Sarangi, Niranjan, and Sashi Kanta Panigrahi. Aero Engine Combustor Casing: Experimental Design and Fatigue Studies. Taylor & Francis Group, 2017.

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30

Sarangi, Niranjan, and Sashi Kanta Panigrahi. Aero Engine Combustor Casing: Experimental Design and Fatigue Studies. Taylor & Francis Group, 2017.

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31

Aero Engine Combustor Casing: Experimental Design and Fatigue Studies. Taylor & Francis Group, 2017.

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32

Moyer, James Ambrose 1875. Power Plant Testing; a Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Materials of Construction, Etc. Creative Media Partners, LLC, 2015.

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33

Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Materials of Construction, Etc. Creative Media Partners, LLC, 2018.

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34

Anonyma. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Materials of Construction, Etc. Franklin Classics, 2018.

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35

Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Materials of Construction, Etc. Creative Media Partners, LLC, 2018.

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36

MODELING OF HIGH-STRAIN-RATE DEFORMATION, FRACTURE, AND IMPACT BEHAVIOR OF ADVANCED GAS TURBINE ENGINE MATERIALS..., NASA/CR--2003-212194... [S.l: s.n., 2003.

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37

Moyer, James Ambrose. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Lubricants, Materials of Construction, Etc. Franklin Classics Trade Press, 2018.

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38

Moyer, James Ambrose. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Lubricants, Materials of Construction, Etc. Creative Media Partners, LLC, 2018.

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39

Moyer, James Ambrose. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Lubricants, Materials of Construction, Etc. Creative Media Partners, LLC, 2022.

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40

Moyer, James Ambrose. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Lubricants, Materials of Construction, Etc. Franklin Classics, 2018.

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41

Moyer, James Ambrose. Power Plant Testing: A Manual of Testing Engines, Turbines, Boilers, Pumps, Refrigerating Machinery, Fans, Fuels, Lubricants, Materials of Construction, Etc. Franklin Classics Trade Press, 2018.

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