17   Artículos

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en línea
Xiaoshuang Han, Weiliang Qiao and Bo Zhou    
This article presents a procedure that simplifies an offshore jacket platform as a non-uniform cantilever beam subjected to an axial force. A Ritz method combined with a pseudo-excitation method is then used to analyze the responses of the jacket platfor... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Feng Gao and Wei Sun    
For the purpose of improving the working reliability of the blisk (integrally-bladed disk) under severe environment, a passive vibration reduction method by depositing a hard coating on both sides of blades is developed and then investigated systematical... ver más
Revista: Coatings    Formato: Electrónico

 
en línea
Abbes Elmeiche, Abdelkader Megueni, Abdelkader Lousdad     Pág. 209 - 219
This paper presents the fundamental frequency analysis of functionally graded (FG) nanobeams using Ritz method subjected to different sets of boundary conditions. The vibration analysis is based on the classical, the first-order and different higher-orde... ver más
Revista: Periodica Polytechnica: Mechanical Engineering    Formato: Electrónico

 
en línea
Afshan Kanwal, Chang Phang and Umer Iqbal    
In this paper, two-dimensional Genocchi polynomials and the Ritz?Galerkin method were developed to investigate the Fractional Diffusion Wave Equation (FDWE) and the Fractional Klein?Gordon Equation (FKGE). A satisfier function that satisfies all the init... ver más
Revista: Computation    Formato: Electrónico

 
en línea
Hui Li, Zhengxue Zhou, Hai Sun, Wei Sun and Bangchun Wen    
The influence of hard coating on vibration characteristics of fiber-reinforced composite thin shell (FCTS) is investigated theoretically. The theoretical model of the hard coating FCTS is firstly established by using the classical laminated shell theory,... ver más
Revista: Coatings    Formato: Electrónico

 
en línea
Andrzej Majka    
Unmanned aircraft must be characterized by a level of safety, similar to that of manned aircraft, when performing flights over densely populated areas. Dangerous situations or emergencies are frequently connected with the necessity to change the profiles... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Afshan Kanwal, Chang Phang and Umer Iqbal    
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Revista: Computation    Formato: Electrónico

 
en línea
Ahmad Nayan and Tai Yan Kam    
A new vibro-acoustic method is presented to analyze the sound radiation behavior of orthotropic panel-form sound radiators using strip-type exciters to exert line loads to the panels for sound radiation. The simple first-order shear deformation theory to... ver más
Revista: Acoustics    Formato: Electrónico

 
en línea
Yun Qin, Qinghua Song, Zhanqiang Liu and Jiahao Shi    
In this paper, the vibration analysis of a partially constrained layer damping plate subjected to moving loads is investigated. In addition, the first four order damping loss factor of the system is optimized with the location of partially constrained la... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Minghui Yi, Fei Liu, Wuxiang Zhang and Xilun Ding    
Variable angle tow steering technology is capable of manufacturing complex aviation parts with a trajectory of intricate curvature planned based on stress or profile characteristics, which greatly improves the forming efficiency, design flexibility and m... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Malgorzata Chwal and Aleksander Muc    
The buckling and free vibrations of rectangular nanoplates are considered in the present paper. The refined continuum transverse shear deformation theory (third and first order) is introduced to formulate the fundamental equations of the nanoplate. Besid... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Aleksander Muc    
Free vibration (or eigenvalue analysis) is a prerequisite for aeroelastic analysis. For divergence analysis, slope influence coefficients (rotation at point i due to unit load at point j) are calculated using free vibration mode shapes and corresponding ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Aleksander Muc    
Free vibration (or eigenvalue analysis) is a prerequisite for aeroelastic analysis. For divergence analysis, slope influence coefficients (rotation at point i due to unit load at point j) are calculated using free vibration mode shapes and corresponding ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Vladimir Karpov, Aleksandr Panin, Alexey Semenov     Pág. 261 - 266
Thin shells are often used for roofing of large-span constructions including hangars for vehicles. This paper considers the approach to study of strength and stability of such structures. A geometrically nonlinear mathematical model of deformation of dou... ver más
Revista: Transportation Research Procedia    Formato: Electrónico

 
en línea
ALI MUHAMMAD    
Terrorism emerged as serious security problem inIndonesia since a network of terrorist group rockedthis country, started from the Bali bombing (2002)followed by other consecutive bombings, such as, J.W. Marriott Hotel bombing (2003), the AustralianEmbass... ver más
Revista: Journal of Government and Politics    Formato: Electrónico

 
en línea
Xiaochun Zhang, Jianhan Hu and Shuyang Chen    
In the southeastern coastal regions of China, thick layers of marine soft soil are widely distributed, exhibiting characteristics such as high compressibility, high porosity, low strength, high sensitivity, and easy thixotropy, and these viscoelastic beh... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Jafar S. Pilakkadan, Rafic M. Ajaj, Zawar Haider and Mohammadreza Amoozgar    
This paper studies the aeroelastic behavior of a rectangular, cantilever wing equipped with the spanwise morphing trailing edge (SMTE) concept. The SMTE consists of multiple trailing edge flaps that allow controlling the spanwise camber distribution of a... ver más
Revista: Aerospace    Formato: Electrónico

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