77 to 1200 K tensile properties of several wrought superalloys after long-term 1093 K heat treatment in air and vacuum-Reference-Cited by-同舟云学术

77 to 1200 K tensile properties of several wrought superalloys after long-term 1093 K heat treatment in air and vacuum

Published:1994-02 Issue:1 Volume:3 Page:91-103
ISSN:1059-9495
Container-title:Journal of Materials Engineering and Performance
language:en
Short-container-title:JMEP

Author:

Whittenberger J. D.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/BF02654504.pdf

Reference9 articles.

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4. H.J. Strumpf, R.P. Rubley, and M.G. Coombs, Material Compatibility and Simulation Testing for the Brayton Engine Solar Receiver for the NASA Space Station Freedom Solar Dynamic Option, Paper No. 899076,IECEC, Vol 2, IEEE, 1989, p 895–903

5. D.T. Bourgette and H.E. McCoy,Trans ASM, Vol 59,1966, p 324–339

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