Table of contents
Analysis of nano‐reinforced layered plates via classical and refined two‐dimensional theories
Salvatore Brischetto, Erasmo CarreraThe purpose of this paper is to consider the static analysis of nanocomposite plates. Nanocomposites consist of a small amount of nanoscale reinforcements which can have an…
Sensitivity of TM nonlinear magnetooptical integrated optical sensor
Hala J. El‐Khozondar, Rifa J. El‐Khozondar, Mathias S. Müller, A.W. KochThe purpose of this paper is to consider a detailed investigation of transversal magnetic (TM) nonlinear magnetooptical integrated optical sensor. The sensitivities of two sensors…
Three‐dimensional quantification of the manufacturing defects for tolerances analysis
Maher Barkallah, Karim Jaballi, Jamel Louati, Mohamed HaddarThe purpose of this paper is to present an experimental approach to measure and quantify the three‐dimensional geometrical manufacturing errors on a mass production of parts.
Propagation of waves at an imperfect boundary between heat conducting micropolar thermoelastic solid and fluid media
Rajneesh Kumar, Mandeep Kaur, S.C. RajvanshiThe purpose of this paper is to establish a mathematical model to investigate the propagation of waves at an imperfect boundary between heat conducting micropolar elastic solid…
The parametered modeling technology study for the civil aircraft engine fan blade
Haijun Zeng, Youchao SunThe purpose of this paper is to introduce parametered modeling technology for the civil aircraft engine fan blade, to design the fan blade rapidly and accurately.
Basic models of isothermal depolarization analysis for diagnostics of heterogeneous materials
V.S. Khandetskyi, Yury A. TonkoshkurThe purpose of this paper is to explore and develop specific models of the kinetics of isothermal depolarization currents (IDC) and the corresponding methods for the diagnostics…
Fatigue life reliability based design optimization for the missile suspension structure
ZhiQun Liu, YiShang Zhang, WenBo WangThe purpose of this paper is to optimize the key dimensions parameters of the missile suspension structure to ensure the structural fatigue life (>10000 cycles) with the…
ISSN:
1573-6105e-ISSN:
1573-6113ISSN-L:
1573-6105Online date, start – end:
2005Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditors:
- Dr Xiao-Ping Zhang
- Professor Zhufeng Yue
- Prof Heng Xiao