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Book Modeling of High Strain Rate Deformation  Fracture  and Impact Behavior of Advanced Gas Turbine Engine Materials at Low and Elevated Temperatures

Download or read book Modeling of High Strain Rate Deformation Fracture and Impact Behavior of Advanced Gas Turbine Engine Materials at Low and Elevated Temperatures written by and published by DIANE Publishing. This book was released on 2003 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Modeling of High Strain Rate Deformation  Fracture  and Impact Behavior of Advanced Gas Turbine Engine Materials at Low and Elevated Temperatures

Download or read book Modeling of High Strain Rate Deformation Fracture and Impact Behavior of Advanced Gas Turbine Engine Materials at Low and Elevated Temperatures written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-03 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Gamma titanium aluminides have received considerable attention over the last decade. These alloys are known to have low density, good high temperature strength retention, and good oxidation and corrosion resistance. However, poor ductility and low fracture toughness have been the key limiting factors in the full utilization of these alloys. More recently, Gamma-met PX has been developed by GKSS, Germany. These alloys have been observed to have superior strengths at elevated temperatures and quasi-static deformation rates and good oxidation resistance at elevated temperatures when compared with other gamma titanium aluminides. The present paper discusses results of a study to understand dynamic response of gamma-met PX in uniaxial compression. The experiments were conducted by using a modified split Hopkinson pressure bar between room temperature and 900 C and strain rates of up to 3500 per second. The Gamma met PX alloy showed superior strength when compared to nickel based superalloys and other gamma titanium aluminides at all test temperatures. It also showed strain and strain-rate hardening at all levels of strain rates and temperatures and without yield anomaly up to 900 C. After approximately 600 C, thermal softening is observed at all strain rates with the rate of thermal softening increasing dramatically between 800 and 900 C. However, these flow stress levels are comparatively higher in Gamma met PX than those observed for other TiAl alloys.Shazly, Mostafa and Nathenson, David and Prakash, VikasGlenn Research CenterGAS TURBINE ENGINES; LOW TEMPERATURE; STRAIN RATE; DEFORMATION; FRACTURE MECHANICS; HIGH TEMPERATURE TESTS; MATHEMATICAL MODELS; IMPACT TESTS; MECHANICAL PROPERTIES; STRESS-STRAIN DIAGRAMS; MICROSTRUCTURE; INTERMETALLICS; LOAD TESTS; SABOT PROJECTILES; VELOCITY DISTRIBUTION; THERMOCOUPLES; TITANIUM ALUMINIDES; TENSILE TESTS

Book Modeling of High strain rate Deformation  Fracture  and Impact Behavior of Advanced Gas Turbine Engine Materials      Nasa cr  2003 212194

Download or read book Modeling of High strain rate Deformation Fracture and Impact Behavior of Advanced Gas Turbine Engine Materials Nasa cr 2003 212194 written by United States. National Aeronautics and Space Administration and published by . This book was released on 2003* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book High Strain Rate Behavior of Nanocomposites and Nanocoatings

Download or read book High Strain Rate Behavior of Nanocomposites and Nanocoatings written by Prashant Jindal and published by Springer. This book was released on 2014-12-30 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book describes the use of multiwall carbon nanotubes as composites with polycarbonates and as protective coatings on glass surfaces. The book explains fabrication and characterization methods for these composites and coatings. The author reports on the use of Split Hopkinson Pressure Bar set up for evaluating the dynamic strength of these composites and coatings and studying the role of carbon nanotubes in the enhancement of their dynamic strength.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1988 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1992 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book International Aerospace Abstracts

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 1042 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Publications of the National Institute of Standards and Technology     Catalog

Download or read book Publications of the National Institute of Standards and Technology Catalog written by National Institute of Standards and Technology (U.S.) and published by . This book was released on 1991 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Metals Abstracts

Download or read book Metals Abstracts written by and published by . This book was released on 1998 with total page 1076 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Creep

    Book Details:
  • Author : Tomasz Tański
  • Publisher : BoD – Books on Demand
  • Release : 2018-01-10
  • ISBN : 9535137247
  • Pages : 270 pages

Download or read book Creep written by Tomasz Tański and published by BoD – Books on Demand. This book was released on 2018-01-10 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book contains 12 chapters with original and innovative research studies in the issues related to the broadly defined creep effect, which concerns not only the area of construction materials but also natural phenomena. The emphasis on the discussion of a new trend of experimental creep testing, which binds the classic creep methods to seek the correlation of parameters obtained in tests, deserves particular attention. This book aims to provide the readers, including, but not limited to, students and doctoral students and also the research personnel and engineers involved in the operation of equipment and structural components as well as specialists in high-temperature creep-resisting materials, with a comprehensive review of new trends in the field of creep-exposed materials and their research methodology. The chapters of this book were developed by respected and well-known researchers from different countries.

Book Engine Structures

Download or read book Engine Structures written by and published by . This book was released on 1988 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Metals Abstracts Index

Download or read book Metals Abstracts Index written by and published by . This book was released on 1995 with total page 1390 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Engineered Materials Abstracts

Download or read book Engineered Materials Abstracts written by and published by . This book was released on 1995-10 with total page 496 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cracks in superalloys

    Book Details:
  • Author : Jonas Saarimäki
  • Publisher : Linköping University Electronic Press
  • Release : 2018-01-18
  • ISBN : 9176853853
  • Pages : 63 pages

Download or read book Cracks in superalloys written by Jonas Saarimäki and published by Linköping University Electronic Press. This book was released on 2018-01-18 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt: Gas turbines are widely used in industry for power generation and as a power source at hard to reach locations where other possibilities for electrical power supplies are insufficient. New ways of producing greener energy is needed to reduce emission levels. This can be achieved by increasing the combustion temperature of gas turbines. High combustion temperatures can be detrimental and degrade critical components. This raises the demands on the high temperature performance of the superalloys used in gas turbine components. These components are frequently subjected to different cyclic loads combined with for example dwell-times and overloads at elevated temperatures, which can influence the crack growth. Dwell-times have been shown to accelerate crack growth and change cracking behaviour in both Inconel 718, Haynes 282 and Hastelloy X. On the other hand, overloads at the beginning of a dwell-time cycle have been shown to retard the dwell-time effect on crack growth in Inconel 718. More experiments and microstructural investigations are needed to better understand these effects. The work presented in this thesis was conducted under the umbrella of the research program Turbo Power; "High temperature fatigue crack propagation in nickel-based superalloys", where I have mainly looked at fatigue crack growth mechanisms in superalloys subjected to dwell-fatigue, which can have a devastating effect on crack propagation behaviour. Mechanical testing was performed under operation-like cycles in order to achieve representative microstructures and material data for the subsequent microstructural work. Microstructures were investigated using light optical microscopy and scanning electron microscopy (SEM) techniques such as electron channeling contrast imaging (ECCI) and electron backscatter diffraction (EBSD). The outcome of this work has shown that there is a significant increase in crack growth rate when dwell-times are introduced at maximum load (0 % overload) in the fatigue cycle. With the introduction of a dwell-time there is also a shift from transgranular to intergranular crack growth for both Inconel 718 and Haynes 282. The crack growth rate decreases with increasing overload levels in Inconel 718 when an overload is applied prior to the dwell-time. At high temperature, intergranular crack growth was observed in Inconel 718 as a result of oxidation and the creation of nanometric voids. Another observed growth mechanism was crack advance along ?-phase boundaries with subsequent oxidation of the ?-phase. This thesis comprises two parts. Part I gives an introduction to the field of superalloys and the acting microstructural mechanisms related to fatigue and crack propagation. Part II consists of five appended papers, which report the work completed as part of the project.

Book Indexes to     Publications

Download or read book Indexes to Publications written by American Society of Mechanical Engineers and published by . This book was released on 1978 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt: