Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Hesham Hamed Ibrahim"'
Publikováno v:
2021 13th International Conference on Computer and Automation Engineering (ICCAE).
The current work provides data based modeling of passive automotive suspension dynamics of a half-car model, by implementing different machine learning techniques, which model the passive dynamics. The passive vertical and pitch suspension dynamics,
Publikováno v:
VEHITS
Publikováno v:
VEHITS
Publikováno v:
NILES
This paper presents an identification technique, for the road - vehicle dynamic behavior of suspension systems, by implementing an autoregressive system with exogenous input (ARX). The ARX model was proposed as a simple and powerful tool, in terms of
Publikováno v:
XI International Conference on Structural Dynamics.
Publikováno v:
XI International Conference on Structural Dynamics.
Publikováno v:
Journal of Physics: Conference Series. 1264:012048
A Finite Element model for variable cross section offshore wind turbine with flexible foundation is developed to accurately determine the fundamental frequency of the tower-nacelle system. The tower is modeled using two-noded Euler beam element with
Publikováno v:
Journal of Physics: Conference Series. 1264:012049
A new semi analytical formulation is developed which models the dynamic behavior of offshore wind turbine with variable cross section and flexible foundation. The wind turbine tower is modeled using Euler-Bernoulli beam model while the soil-tower int
Publikováno v:
Journal of Physics: Conference Series. 1264:012019
This work presents hands on experience of the configuration process and strength analyses of a student’s CubeSat project at the German University in Cairo. The static and dynamic performance of the primary structure, during launching phase, are inv
Publikováno v:
Journal of Vibration and Control. 17:321-333
A new nonlinear finite element model is provided for the nonlinear flutter response of shape memory alloy (SMA) hybrid composite plates under the combined effect of thermal and aerodynamic loads. The nonlinear governing equations for moderately thick