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Incinerators, materials selection

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Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001046
EISBN: 978-1-62708-214-3
... confirmed the suitability of the nickel-chromium alloys for such an environment. Inconel 625 was selected for fabrication of a new preheater/exchanger. Heat exchangers, materials selection Incinerators, materials selection Internal oxidation Nickel-base alloys, corrosion Solvents, environment 309...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003555
EISBN: 978-1-62708-180-1
...-Temperature Corrosion , Oxid. Met. , Vol 44 , 1995 , p 177 21. Smith R.A. , Corrosion , 2nd ed. , Sheir L.L. , Ed., Newes-Butterworths , London , 1976 , p 7 : 90 22. Materials of Construction for Shipboard Waste Incinerators , National Research Council, National Academy...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006787
EISBN: 978-1-62708-295-2
... 24. Materials of Construction for Shipboard Waste Incinerators , National Research Council, National Academy of Sciences , 1977 , p 91 – 92 25. Hatfield W.H. , Heat Resisting Steels , J. Iron Steel Inst. , Vol 115 , 1927 , p 483 26. Wright I.G. , High Temperature...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001834
EISBN: 978-1-62708-241-9
... – 1029 ( 2009 ) 10.1016/j.corsci.2009.02.025 15. French D.N. , Metallurgical Failures in Fossil Fired Boilers ( Wiley , New York , 2000 ) 16. Kawahara Y. , High temperature corrosion mechanisms and effect of alloying elements for materials used in waste incineration...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006821
EISBN: 978-1-62708-329-4
... , 8 ). In aircraft design, it is important to understand the environment in which the aircraft will be operating and the stresses it will need to be capable of withstanding, because these conditions will dictate size, shape, materials selection, and so on for each component of the aircraft...