Inicio  /  SCRIPTA MATERIALIA  /  Vol: 55 Núm: 2 Par: 0 (2006)  /  Artículo
ARTÍCULO
TITULO

Internal stress evolution in a random-planar short fiber aluminum composite

Gerardo Garces    
Giovanni Bruno and Alexander Wanner    

Resumen

No disponible

 Artículos similares

       
 
Abdul Basit, Safeer Abbas, Muhammad Mubashir Ajmal, Ubaid Ahmad Mughal, Syed Minhaj Saleem Kazmi and Muhammad Junaid Munir    
This study undertakes a comprehensive experimental and numerical analysis of the structural integrity of buried RC sewerage pipes, focusing on the performance of two distinct jointing materials: cement mortar and non-shrinkage grout. Through joint shear ... ver más
Revista: Infrastructures

 
Songyang Wang, Jianjun Ma, Chaosheng Wang, Fengjun Liu and Da Li    
The scouring effect is widely acknowledged as a primary contributor to the weakening in the bearing performance of offshore piles; it often results in asymmetric scour patterns around the pile. To meticulously examine the impact of three-dimensional asym... ver más
Revista: Applied Sciences

 
Isehaq Al-Huseini, Maryam Al-Ismaili, Ammar Boudaka and Srinivasa Rao Sirasanagandla    
Vascular calcification is calcium deposition occurring in the wall of blood vessels, leading to mechanical stress and rupture due to a loss of elasticity and the hardening of the vessel wall. The role of the Transient Receptor Channel Vanilloid 4 (TRPV4)... ver más
Revista: Applied Sciences

 
Zhe Mei, Anfeng Xiao, Jiahao Mei, Jinqiu Hu and Peng Zhang    
In order to study the variation law of shear frictional characteristics of the steel pipe jacking and sand interface under different working conditions, the shear stress?strain curve between five different particle sizes of sand and steel pipe jacking un... ver más
Revista: Applied Sciences

 
Weiwei Sun, Yue Liu, Qi An, Shouqing Huang and Fangyong Li    
Multilayer insulation (MLI) components are important parts of spacecraft, in which thin films are the core elements. The film thicknesses are generally small, between 10 and 30 µm, to reduce the weight of the spacecraft. During the launch of a spacecraft... ver más
Revista: Aerospace