Tuning the stress state in Nb-thin films by lateral size confinement

2021 ◽  
pp. 117454
Author(s):  
Philipp Klose ◽  
Vladimir Roddatis ◽  
Astrid Pundt
2015 ◽  
Vol 51 (91) ◽  
pp. 16385-16388 ◽  
Author(s):  
Zhao Yuan ◽  
Yu Shu ◽  
Yu Tian ◽  
Yan Xin ◽  
Biwu Ma

We report a facile one-pot synthetic method to prepare highly luminescent layered lead(ii) bromide perovskite microdisks with the lateral size of a few micrometers and thickness of 100–150 nm, featuring narrow deep blue emissions with quantum yields of up to 53% in toluene solutions and thin films at room temperature.


2014 ◽  
Vol 306 ◽  
pp. 70-74 ◽  
Author(s):  
D. Faurie ◽  
P.-O. Renault ◽  
E. Le Bourhis ◽  
G. Geandier ◽  
P. Goudeau ◽  
...  

2014 ◽  
Vol 47 (1) ◽  
pp. 291-302 ◽  
Author(s):  
Silke Julia Birgit Kurz ◽  
Udo Welzel ◽  
Ewald Bischoff ◽  
Eric Jan Mittemeijer

The presence of planar faults complicates the diffraction stress analysis enormously owing to fault-induced displacement, broadening and asymmetry of the Bragg reflections. A dedicated stress-analysis method has been developed for highly planar-faulted, fibre-textured thin films of cubic crystal symmetry, using only specific reflections for diffraction stress analysis. The effect of unjustified use of other reflections has been demonstrated in the course of application of the method to Ni and Ni(W) thin films exhibiting excessive faulting and subjected to (1) a planar, rotationally symmetric stress state and (2) a planar biaxial stress state. In case 1 the crystallite-group method has been used, whereas in case 2 the stress-analysis method based on X-ray stress factors had to be applied. The successful separation of stress- and fault-induced reflection displacements has enabled the investigation of the mechanical behaviour of Ni and Ni(W) thin films byin situstress measurements during tensile loading, thereby exposing pronounced stiffness and increased strength by alloying with W.


The mechanics of delamination from an edge flaw in a laminated material is presented. Two different types of failure mechanism have been identified: uniform delamination along the crack front and localized delamination which can be initiated if the laminate buckles above the debonded portion of the interface. Depending on the stress state within the bonded portion of the laminate, this localized failure can initiate the formation of blisters which grow by a mechanism of buckling-driven delamination and can cause general failure of the laminate. There are conditions under which this class of buckling-assisted delamination occurs at loads lower than would be predicted for uniform delamination. It may, therefore, have important implications in the design against failure for thin films, composites and other laminated systems. Experimental observations of the different failure mechanisms are presented and the factors governing the transitions between them are discussed.


2013 ◽  
Vol 530 ◽  
pp. 25-29 ◽  
Author(s):  
D. Faurie ◽  
G. Geandier ◽  
P.-O. Renault ◽  
E. Le Bourhis ◽  
D. Thiaudière
Keyword(s):  

2003 ◽  
Vol 42 (Part 1, No. 1) ◽  
pp. 270-273 ◽  
Author(s):  
Hiroyuki Nasu ◽  
Hiroshi Iwatani ◽  
Takafumi Iwano ◽  
Tadanori Hashimoto ◽  
Kanichi Kamiya

2004 ◽  
Vol 71 (5) ◽  
pp. 597-603 ◽  
Author(s):  
X. Chen ◽  
John W. Hutchinson

A thin metal film vapor deposited on thick elastomer substrate develops an equi-biaxial compressive stress state when the system is cooled due to the large thermal expansion mismatch between the elastomer and the metal. At a critical stress, the film undergoes buckling into a family of modes with short wavelengths characteristic of a thin plate on a compliant elastic foundation. As the system is further cooled, a highly ordered herringbone pattern has been observed to develop. Here it is shown that the herringbone mode constitutes a minimum energy configuration among a limited set of competing modes.


Vacuum ◽  
1977 ◽  
Vol 27 (3) ◽  
pp. 109-117 ◽  
Author(s):  
RN Castellano ◽  
MR Notis ◽  
GW Simmons

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