Properties of a TZP/Al2O3 Composite After Long-Term Exposure at 1000 Deg C. PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Properties of a TZP/Al2O3 Composite After Long-Term Exposure at 1000 Deg C. PDF full book. Access full book title Properties of a TZP/Al2O3 Composite After Long-Term Exposure at 1000 Deg C. by . Download full books in PDF and EPUB format.
Author: Publisher: ISBN: Category : Languages : en Pages : 19
Book Description
A commercially available tetragonal zirconia polycrystal ceramic was examined for potential use in advanced engines. Room temperature strength and toughness were determined, as well as the static fatigue life between 800 deg C and 1200 deg C. All of these properties were determined before and after a 100 hour exposure at 1000 deg C. The room temperature flexure strength was 1838 MPa before exposure and it decreased 23% after exposure. The toughness did not change with the exposure. Static fatigue testing revealed that fracture below 1100 deg C was due to the cracks created during machining. At 1100 deg C and higher slow crack growth became the dominant failure mechanism. Overall, the high temperature static fatigue life is better than yttria tetragonal zirconia polycrystal materials without Alumina but it still does not meet the strength at temperature requirements for use in advanced engines.
Author: Publisher: ISBN: Category : Languages : en Pages : 19
Book Description
A commercially available tetragonal zirconia polycrystal ceramic was examined for potential use in advanced engines. Room temperature strength and toughness were determined, as well as the static fatigue life between 800 deg C and 1200 deg C. All of these properties were determined before and after a 100 hour exposure at 1000 deg C. The room temperature flexure strength was 1838 MPa before exposure and it decreased 23% after exposure. The toughness did not change with the exposure. Static fatigue testing revealed that fracture below 1100 deg C was due to the cracks created during machining. At 1100 deg C and higher slow crack growth became the dominant failure mechanism. Overall, the high temperature static fatigue life is better than yttria tetragonal zirconia polycrystal materials without Alumina but it still does not meet the strength at temperature requirements for use in advanced engines.
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 168
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Author: Publisher: ISBN: Category : Languages : en Pages : 25
Book Description
Seven commercially available yttria-tetragonal zirconia polycrystal (Y-TZP) materials were evaluated. Room temperature properties were measured before and after heat treatments at 1000C. Microstructure and phase stability were also examined. In all but one case, the Y-TZPs showed very little change in room temperature properties after long times at this temperature. Results show that pressure-assisted processing greatly improves the strength by reducing porosity and keeping the grain size extremely fine, but this reduces the toughness because finer grains are more difficult to transform. In addition, a small amount of cubic zirconia appears to enhance the toughness of fine-grained Y-TZP while maintaining good strength. During processing, a small amount of cubic zirconia is formed and allowed to grow. This creates regions poor in yttria which can transform spontaneously in the presence of a crack-tip stress field.
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: