Low-temperature fracture resistance of asphalt mixtures modified with carbon nanotubes

Author(s):  
Ali Mansourkhaki ◽  
Amir Aghasi
2010 ◽  
Vol 22 (2) ◽  
pp. 145-152 ◽  
Author(s):  
Xinjun Li ◽  
Mihai O. Marasteanu ◽  
Andrea Kvasnak ◽  
Jason Bausano ◽  
R. Christopher Williams ◽  
...  

2012 ◽  
Vol 24 (8) ◽  
pp. 1089-1096 ◽  
Author(s):  
Eyoab T. Zegeye ◽  
Ki H. Moon ◽  
Mugur Turos ◽  
Timothy R. Clyne ◽  
Mihai O. Marasteanu

2002 ◽  
Vol 1789 (1) ◽  
pp. 191-199 ◽  
Author(s):  
Mihai O. Marasteanu ◽  
Shongtao Dai ◽  
Joseph F. Labuz ◽  
Xue Li

1996 ◽  
Vol 434 ◽  
Author(s):  
R. G. Rowe ◽  
D. W. Skelly ◽  
M. R. Jackson ◽  
M. Larsen ◽  
D. Lachapelle

AbstractHigher gas path temperatures for greater aircraft engine thrust and efficiency will require both higher temperature gas turbine airfoil materials and optimization of internal cooling technology. Microlaminated composites consisting of very high temperature intermetallic compounds and ductile refractory metals offer a means of achieving higher temperature turbine airfoil capability without sacrificing low temperature fracture resistance. Physical vapor deposition, used to synthesize microlaminated composites, also offers a means of fabricating advanced turbine blade internal cooling designs. The low temperature fracture resistance of microlaminated Nb(Cr)-Cr2Nb microlaminated composites approached 20 MPa√m in fracture resistance curves, but the fine grain size of vapor deposited intermetallics indicates a need to develop creep resistant microstructures.


2017 ◽  
Vol 18 (sup4) ◽  
pp. 467-490 ◽  
Author(s):  
Yuefeng Zhu ◽  
Eshan V. Dave ◽  
Reyhaneh Rahbar-Rastegar ◽  
Jo Sias Daniel ◽  
Adam Zofka

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