دانلود فایل مرور مقالات پژوهشی درباره توربولاتورها یا تولید کننده های آشفتگی در کلکتورهای خورشیدی به زبان فارسی

در این فایل 67 صفحه ای مروری بر 60 منبع موجود تا سال 2022 در زمینه آشفته سازها یا توبولاتورها در کلکتورهای خورشیدی انجام گرفته است. مطالعه آن برای افراد علاقمند به افزایش راندمان کلکتورهای خورشیدی و تهیه سمینار و نوشتن پایان نامه در این زمینه اکیدا توصیه می شود.

دانلود پایان نامه انگلیسی تولید قطره در مقیاس نانولیتر تا فمتولیتر Droplet Generation From the Nanoliter to the Femtoliter Range

This thesis provides a general description of micro droplet generation at low and
medium Weber numbers using analytical, numerical and experimental methods in an
engineering manner of contemplation. Based on the presented results guidelines are
deduced to support the designing and operating any type of micro droplet generator.

دانلود پایان نامه انگلیسی دربارۀ ایرودینامیک توربین بادی

This thesis hence aims to improve our understanding of rotor aerodynamics
in yaw using wind tunnel experiments. Its concrete objectives are:
quantify the effects of experimentally observed yaw misalignment on
rotor inflow and blade loads
• identify the aerodynamic mechanisms governing the effects of yaw misalignment
on rotor inflow and blade loads
• assess the validity of semi-empirical submodels, used to patch BEMtheory;
the Glauert momentum equation for yaw, induction non-uniformity
corrections in yaw, airfoil dynamic stall models.

دانلود پایان نامه کارشناسی ارشد انگلیسی دربارۀ مطالعه عددی تشکیل قطره به روش لتیس-بولتزمن Lattice Boltzmann Method

Liquid droplets are widely used as reaction media for the chemical manipulation of cells. The droplet formation and cell encapsulation process involves multiphase flows along with coupled cell membrane-fluid mechanics. In this study, the droplet formation behavior in a T-shaped micro-fluidic device is simulated using two- and three-dimensional lattice Boltzmann method (LBM). With the adoption of pseudo potential model, the LBM can accomplish the accurate tracking of the liquid-liquid or liquid-gas interface automatically. The two-dimensional simulation results agree favorably with experimental results in the aspects of droplet length and the droplet shapes before and after the breakup. For the two-dimensional cell model, the effects of the two important dimensionless parameters, the shear rate and the reduced ratio of bending to elasticity moduli, are investigated systematically. The deformation of the cell in the process of cell encapsulation is found to have close relation with the local flow flied. Surprisingly, it is found that, the cell is still experiencing the force from the surrounding fluid even when the steady transportation of the cell has started after it has been capsulated in a droplet. In the three-dimensional simulations, three regimes of droplet formation are clearly identified as the capillary number increases from 0.002 to 0.056. The previously known four stages of squeezing regime are reproduced.

دانلود پایان نامه انگلیسی میدان جریان و انتقال حرارت در دسته میله ها Rod Bundles

Prcsentcd in this study is an investigation of nirbulcnt flow and heat transfcr near
narrow gaps of rod bundlcs. At first. practical crnpirical corrclations for the subchanncl
avcragc and thc gay, local hcat transfer coeficicnts wcrc fincd to cxperimcntal I-csults
availablc in the literaturc. Then. thc thcsis prcsents a new technique. using a pcndulum. for
thc calibration of hot-wirc ancmomctcrs ovcr low vclocity ranges. a signal analysis
procedurc for thrce-sensor hot-wirc probes. and a mcthod for thc cnhancemcnt of the rcsults
of the Variable Interval Timc Average (VITA) conditional sampling technique. al1 used in
the main cxperimcntal snidy.

دانلود پایان نامه انگلیسی آنالیز، تولید و تست یک سیستم میکروپیشرانش بر پایه میکروالکترومکانیکال سیستم ها

Various trends in the spacecraft industry are driving the development of low-thrust propulsion systems.
These may be needed for fine attitude control, or to reduce the mass of the propulsion system through the
use of small lightweight components. The nozzle converts the stored energy in a pressurized gas into kinetic
energy through an expansion. The nozzle efficiency is characterized by the amount of kinetic energy leaving
the nozzle, and is governed by the exit velocity. Because of the increase in viscous losses as scale is reduced,
it was feared that high Mach number supersonic flows could not be generated in microdevices. However, a
scaling analysis indicates that the reduction in throat area can be offset by an increase in operating pressure
to maintain a constant Reynolds number. Therefore, thrust can be decreased by reducing the nozzle scale,
and viscous losses mitigated by running at higher chamber pressures.

دانلود پایان نامه انگلیسی کارشناسی طراحی یک سیستم هیبریدی تبدیل انرژی بادی-خورشیدی کوچک

Approaching problems with global warming due to
the use of fossil fuels, means that new system
solutions have to be investigated. This report
investigates the possibility to expand an existing
photovoltaic system with a wind turbine
generator to simplify the expansion of renewable
energy sources. Through an extensive literature
study and simulation in SIMULINK the result has
been developed and tested. It shows that it is
possible to connect a wind turbine generator to
the same inverter as the PV-modules if no MPPT
algorithm for PV-modules is integrated. To protect
the inverter a dump load has to be connected.
Because of the complexity a DC-coupled system
brings, AC-coupling is advised when expanding PVmodules
with a WTG. The optimal wind turbine is
considered to be a permanent magnet
synchronous generator connected to the AC-bus
through a full-effect inverter. The turbine should
be chosen according to the intended location
based on wind conditions and desired energy
production.