Abstract: This paper illustrates the study of three isolated zero
voltage switched (ZVS) PWM full bridge (FB) converters to charge
the high voltage battery in the charger of electric vehicle (EV).
EV battery chargers have several challenges such as high efficiency,
high reliability, low cost, isolation, and high power density. The
cost of magnetic and filter components in the battery charger is
reduced when switching frequency is increased. The increase in the
switching frequency increases switching losses. ZVS is used to reduce
switching losses and to operate the converter in the battery charger
at high frequency. The performance of each of the three converters
is evaluated on the basis of ZVS range, dead times of the switches,
conduction losses of switches, circulating current stress, circulating
energy, duty cycle loss, and efficiency. The limitations and merits of
each PWM FB converter are reviewed. The converter with broader
ZVS range, high efficiency and low switch stresses is selected for
battery charger applications in EV.
Abstract: This paper focuses on the study of DC-to-DC
converters, which are suitable for low-voltage high-power
applications. The output voltages generated by renewable energy
sources such as photovoltaic arrays and fuel cell stacks are
generally low and required to be increased to high voltage levels.
Development of DC-to-DC converters, which provide high step-up
voltage conversion ratios with high efficiencies and low voltage
stresses, is one of the main issues in the development of renewable
energy systems. A procedure for three converters−conventional
DC-to-DC converter, interleaved boost converter, and isolated flyback
based converter, is illustrated for a given set of specifications. The
selection among the converters for the given application is based on
the voltage conversion ratio, efficiency, and voltage stresses.
Abstract: This research paper presents the CFD analysis of
oscillating airfoil during pitch cycle. Unsteady subsonic flow is
simulated for pitching airfoil at Mach number 0.283 and Reynolds
number 3.45 millions. Turbulent effects are also considered for this
study by using K-ω SST turbulent model. Two-dimensional unsteady
compressible Navier-Stokes code including two-equation turbulence
model and PISO pressure velocity coupling is used. Pressure based
implicit solver with first order implicit unsteady formulation is used.
The simulated pitch cycle results are compared with the available
experimental data. The results have a good agreement with the
experimental data. Aerodynamic characteristics during pitch cycles
have been studied and validated.