000 | 01531nmm a2200169Ia 4500 | ||
---|---|---|---|
008 | 220920s9999||||xx |||||||||||||| ||und|| | ||
020 | _a9780511541285 | ||
082 |
_a620.161 7 _bR251S |
||
100 |
_aReed, R .C. _eAuthor _lEnglish _92170 |
||
245 | 4 |
_aThe Superalloys _b: Fundamentals and Applications _c/ by R .C. Reed. _h[Electronic Resource] |
|
260 |
_aCambridge _b: Cambridge University Press, _c2006 |
||
300 | _axiv, 372p. | ||
520 | _aSuperalloys are unique high-temperature materials used in gas turbine engines, which display excellent resistance to mechanical and chemical degradation. This book presents the underlying metallurgical principles which have guided their development and practical aspects of component design and fabrication from an engineering standpoint. The topics of alloy design, process development, component engineering, lifetime estimation and materials behaviour are described, with emphasis on critical components such as turbine blading and discs. The first introductory text on this class of materials, it will provide a strong grounding for those studying physical metallurgy at the advanced level, as well as practising engineers. Included at the end of each chapter are exercises designed to test the reader's understanding of the underlying principles presented. Solutions for instructors and additional resources are available at www.cambridge | ||
650 |
_aEngineering _9406 |
||
856 |
_uhttps://doi.org/10.1017/CBO9780511541285 _qPDF _yClick to Access the Online Book |
||
942 |
_cEBK _nYes |
||
999 |
_c12357 _d12357 |