Mesoscopic Structural Length Scales in P3HT/PCBM Mixtures Remain Invariant for Various Processing Conditions

2013 ◽  
Vol 25 (14) ◽  
pp. 2812-2818 ◽  
Author(s):  
Sameer Vajjala Kesava ◽  
Rijul Dhanker ◽  
Derek R. Kozub ◽  
Kiarash Vakhshouri ◽  
U Hyeok Choi ◽  
...  
Coral Reefs ◽  
2012 ◽  
Vol 31 (3) ◽  
pp. 741-752 ◽  
Author(s):  
C. Brahmi ◽  
I. Domart-Coulon ◽  
L. Rougée ◽  
D. G. Pyle ◽  
J. Stolarski ◽  
...  

2014 ◽  
Vol 39 (15) ◽  
pp. 4290 ◽  
Author(s):  
Lusik Cherkezyan ◽  
Hariharan Subramanian ◽  
Vadim Backman

2003 ◽  
Vol 791 ◽  
Author(s):  
Christopher A. Schuh ◽  
David T. Schoen ◽  
Alan C. Lund

ABSTRACTDuring processes of mechanical alloying the characteristic structural length scales of an alloy, including the phase domain size and the crystallite grain size, decrease gradually to a nanocrystalline or even amorphous final state. This method therefore allows a unique avenue to explore the structure-property relationship over several orders of magnitude in length scale. In this work we have considered an ideal equiatomic Ti-Zr system deformed through multiple cold-rolling passes to refine the structural length scales into the nanometer range. The variation of the hardness of the system with decreasing length scale is discussed in terms of traditional Hall-Petch scaling, chemical mixing and the phase evolution of the system, as well as other possible contributions to the hardness variations during processing.


Soft Matter ◽  
2011 ◽  
Vol 7 (11) ◽  
pp. 5255 ◽  
Author(s):  
Ivan Coluzza ◽  
Barbara Capone ◽  
Jean-Pierre Hansen

Soft Matter ◽  
2020 ◽  
Vol 16 (2) ◽  
pp. 289-306 ◽  
Author(s):  
Alejandro G. Marangoni ◽  
John P. M. van Duynhoven ◽  
Nuria C. Acevedo ◽  
Reed A. Nicholson ◽  
Ashok R. Patel

Structural length scales within a fat crystal network, from TAG molecules packing into lamellae, crystalline nanoplatelets and fractal aggregates of nanoplatelets.


Author(s):  
Peter Pegler ◽  
N. David Theodore ◽  
Ming Pan

High-pressure oxidation of silicon (HIPOX) is one of various techniques used for electrical-isolation of semiconductor-devices on silicon substrates. Other techniques have included local-oxidation of silicon (LOCOS), poly-buffered LOCOS, deep-trench isolation and separation of silicon by implanted oxygen (SIMOX). Reliable use of HIPOX for device-isolation requires an understanding of the behavior of the materials and structures being used and their interactions under different processing conditions. The effect of HIPOX-related stresses in the structures is of interest because structuraldefects, if formed, could electrically degrade devices.This investigation was performed to study the origin and behavior of defects in recessed HIPOX (RHIPOX) structures. The structures were exposed to a boron implant. Samples consisted of (i) RHlPOX'ed strip exposed to a boron implant, (ii) recessed strip prior to HIPOX, but exposed to a boron implant, (iii) test-pad prior to HIPOX, (iv) HIPOX'ed region away from R-HIPOX edge. Cross-section TEM specimens were prepared in the <110> substrate-geometry.


1997 ◽  
Vol 473 ◽  
Author(s):  
Michael Lane ◽  
Robert Ware ◽  
Steven Voss ◽  
Qing Ma ◽  
Harry Fujimoto ◽  
...  

ABSTRACTProgressive (or time dependent) debonding of interfaces poses serious problems in interconnect structures involving multilayer thin films stacks. The existence of such subcriticai debonding associated with environmentally assisted crack-growth processes is examined for a TiN/SiO2 interface commonly encountered in interconnect structures. The rate of debond extension is found to be sensitive to the mechanical driving force as well as the interface morphology, chemistry, and yielding of adjacent ductile layers. In order to investigate the effect of interconnect structure, particularly the effect of an adjacent ductile Al-Cu layer, on subcriticai debonding along the TiN/SiO2 interface, a set of samples was prepared with Al-Cu layer thicknesses varying from 0.2–4.0 μm. All other processing conditions remained the same over the entire sample run. Results showed that for a given crack growth velocity, the debond driving force scaled with Al-Cu layer thickness. Normalizing the data by the critical adhesion energy allowed a universal subcriticai debond rate curve to be derived.


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