000 | 01849cam a2200289Ii 4500 | ||
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001 | 9781315116754 | ||
008 | 180331s2017 flu ob 001 0 eng d | ||
020 |
_a9781315116754 _q(e-book : PDF) |
||
020 |
_a9781138032842 _q(e-book: PDF) |
||
020 |
_a9781351633512 _q(e-book: Mobi) |
||
020 |
_z9781138032835 _q(hardback) |
||
024 | 7 |
_a10.1201/9781315116754 _2doi |
|
035 | _a(OCoLC)992167662 | ||
050 | 4 |
_aTL709.5.C55 _bP36 2017 |
|
082 | 0 | 4 |
_a629.134353 _bP192 |
100 | 1 |
_aPanigrahi, Shashi Kanta, _eauthor. _917095 |
|
245 | 1 | 0 |
_aAero engine combustor casing : _bexperimental design and fatigue studies / _cShashi Kanta Panigrahi, Niranjan Sarangi. |
264 | 1 |
_aBoca Raton : _bTaylor & Francis, a CRC title, part of the Taylor & Francis imprint, a member of the Taylor & Francis Group, the academic division of T&F Informa, plc, _c[2017] |
|
300 | _a1 online resource | ||
505 | 0 | _achapter 1 Introduction -- chapter 2 Fatigue Design Philosophy of an Aero Engine Combustor Casing -- chapter 3 Development of Test Facility and Test Setup -- chapter 4 Manufacturing of an Aero Engine Combustor Casing, the Experimental Evaluation of Its Fatigue Life, and Correlation with Numerical Results -- chapter 5 Reassessment of Fatigue Life of the Modified Combustor Casing -- chapter 6 Safety Test on Modified Combustor Casing -- chapter 7 Effect of Fatigue on the Proof Strength of an Aero Engine Combustor Casing* -- chapter 8 Conclusions. | |
650 | 0 |
_aAircraft gas-turbines _xCombustion chambers _xDesign and construction. _917096 |
|
650 | 0 |
_aAircraft gas-turbines _xCombustion chambers _xMaterials _xFatigue. _917097 |
|
700 | 1 |
_aSarangi, Niranjan, _d1946- _eauthor. _917098 |
|
776 | 0 | 8 |
_iPrint version: _z9781138032835 _w(DLC) 2016048815 |
856 | 4 | 0 |
_uhttps://www.taylorfrancis.com/books/9781315116754 _zClick here to view. |
942 | _cEBK | ||
999 |
_c71425 _d71425 |