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Investigation of Possible Ways to Improve a Quad-rotor Controllability and Agility by Increasing Control Parameters
, M.Sc. Thesis Sharif University of Technology ; Malaek, Mohammad Bagher (Supervisor)
Abstract
In the class of unmanned air vehicles (UAV), there is a class entitled as Quad-rotor that engineers pay much attention due to specific features to them. Main applications of this class are because of vertical take-off and landing capability and high controllability. This class has high controllability in environments with high barriers because of the inherent imbalance. All of the Quad-rotors have already studied, had a fixed structure. So the designer's main focus was on improving the guidance and control systems and almost all forms of linear and nonlinear control methods and fuzzy, adaptive and robust control have been investigated. In this study variable structure is examined instead...
Numerical Study of Film Cooling in a Space Thruster
, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor)
Abstract
In high-performance liquid fuel motors and space thrusters, the combustion chamber and nozzle walls are in contact with the gases caused by high temperature and pressure combustion, making severe thermal loads on the walls. Therefore, these systems require cooling mechanisms. The most common way of cooling in space thrusters is film cooling. This study is a numerical simulation of film cooling in the liquid fuel space thrusters. Numerical and empirical studies have been reviewed in this area and evaluated while conducting studies and results to select an appropriate model for ongoing project studies. Along this path, various fuel and oxidizing thrusters, including oxygen and hydrogen,...
Experimental Study of Plasma Effect on Penetration Flame for Non-Premixed Mixtures of Air and Low Calorific Value Fuels
, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor)
Abstract
This project investigates the effect of plasma on diffusion flame. A Dielectric Barrier Discharge (DBD) plasma actuator has been used to generate plasma, which converts fuel-air non-premixed mixtures into plasma. Then, the effect of plasma on the shape and stability of the diffusion flame composed of fuel and air mixture has been evaluated. This study investigates the laminar flow regime for low calorific value fuels. For this purpose, natural gas fuel (urban methane) has been diluted with N2 and CO2 gases to reduce its calorific value. Then, the diffusion flame is formed from the fuel and air mixture in a laboratory stand. This stand consists of two coaxial tubes made of quartz, fuel flows...
Design, Simulation, and Error Analysis for Guidance Law of a Satellite Launcher
, Ph.D. Dissertation Sharif University of Technology ; Mobed, Mohammad (Supervisor) ; Mohammadi, Ali (Supervisor)
Abstract
The problem of launching a satellite to low earth orbit has been considered. Preliminary concepts such as satellite orbits, launcher missiles and their equations of motion, and traditional methods for guidance of launchers are reviewed first. Then a new method for optimizing the launch trajectory under non-ideal conditions is introduced in which the solution of a known ideal trajectory optimization problem is used as an initial guess for the actual optimization problem. Several methods for guiding a launcher to place a satellite in Earth orbit are presented next; they have been titled as (1) launch path re-computation outside the atmosphere, (2) prediction error minimization, and (3) output...
Study of Injection Process from Bi-Swirl Injector in Supercritical Condition
, M.Sc. Thesis Sharif University of Technology ; Farshchi, Mohammad (Supervisor) ; Mardani, Amir (Co-Advisor)
Abstract
Presently, a wide range of devices operate at supercritical condition. In fact, supercritical condition refers to a condition in which both temperature and pressure of injected fluid exceed the critical point. In the case of modern internal combustion engine, the temperature and pressure of combustion chamber is high enough that can be considered as supercritical condition, whilst the fuel injected may be subcritical or transcritical.It has been widely accepted that in supercritical state, vaporization enthalpy is vanished and there is no distinction between gas and liquid. Hence, only a single state will remain which is neither liquid nor gas and referred to as fluid. Moreover, many...
The Effect of Natural Gas Price on Power Plant Emissions in Iran
, M.Sc. Thesis Sharif University of Technology ; Vesal, Mohammad (Supervisor) ; Mardani, Hassan (Co-Supervisor)
Abstract
This study investigates the effect of changes in natural gas and diesel prices on 〖CO 〗_2 emissions from power plants in Iran. We use annual data of fuel prices (including natural gas, diesel, and fuel oil), efficiency, amount of fuel consumed, and emissions of GHG (mainly carbon dioxide) of all thermal power plants from 1997 to 2023. To find the effect of fuel price fluctuations on emissions, gas and diesel price changes are used on two types of gas power plants (gas and diesel consumers) and diesel power plants (diesel consumers). First, a difference-in-difference (DiD) model is used to evaluate the causal effect of fuel price changes on gas power plant's efficiency and emission intensity...
Numerical Investigation of Combustion of Cryogenic H2-O2 Propellant under Sub-Critical Condition
, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor) ; Farshchi, Mohammad (Supervisor)
Abstract
The present work is concerned with numerical simulation of spray flame for rocket combustor (MASCOTTE A-10 test case at 10 bar pressure) based on cryogen gaseous hydrogen and liquid oxygen at specific condition. This liquid oxygen and gaseous hydrogen single element combustor experiment has been the focus of many numerical studies which is representative of combustion in rocket combustion chamber condition. The purposed strategy relies on hybrid Eulerian-Lagrangian framework that continuous phase is evaluated by Reynolds average Navier-stokes (RANS) equation with quick discretization method and dispersed phase of combustion chamber atmosphere is evaluated by discrete phase method (DPM). To...
LBM Computational Simulation of Oscillations Caused by Formation and Detachment of Drops
, M.Sc. Thesis Sharif University of Technology ; Taeibi Rahni, Mohammad (Supervisor) ; Ebrahimi, Abbas (Supervisor)
Abstract
Formation and detachment of drops are of fundamental importance in studying two-phase flows, such as ink jet printing, emulsion, and spray. Drops are formed under the effects of surface tension forces. After formation, forces like gravity detach the drop from the rest of the fluid. The flow rate is varied from dripping to jetting regime. In this project, formation and detachment of drops were simulated, using LBM with phase field model, which can simulate flows with high-density ratios and is a robust method for applying wetting condition on the walls. Results were validated using single-phase and two-phase flows. After code validation, the oscillations caused by formation and detachment of...
Improving the Measurement of the Chemiluminescence of Methylidyne (CH*)Species with the Help of Thermometry by Soot Pyrometry Method
, M.Sc. Thesis Sharif University of Technology ; Salehi, Mohammad Mahdi (Supervisor) ; Mardani, Amir (Supervisor)
Abstract
This research introduces temperature measurement by a non-intrusive pyrometric method of the ratio of two colors of soot. For pyrometry, the spectral sensitivity of the Nikon D7100 camera was obtained by developing a neural network based on the results of photographing colored papers and their spectrum, and this camera was used for temperature measurement. Based on the dependence of soot radiation on temperature and the spectral sensitivity of the camera, a calibration chart has been extracted on the ratio of the green channel to the red channel of the camera with the soot temperature, which is used to produce the temperature contour using the flame image. The temperature contour of...
Numerical Study of Exhaust Chemical Composition in a Methane DBD Plasma Actuator under Different Operating Conditions
, M.Sc. Thesis Sharif University of Technology ; Mardani, Amir (Supervisor) ; Salehi, Mohammad Mahdi (Supervisor)
Abstract
In this study, numerical simulations of a Dielectric-Barrier Discharge (DBD) plasma actuator are performed to predict its output chemical composition. The plasma actuator is cylindrical, with two coaxial electrodes and a quartz dielectric. The electrical discharge occurs in a pulsed manner around the quartz wall. This device is utilized for methane conversion in plasma-assisted combustion applications. The effects of voltage, frequency, temperature, and relative permeability parameters on methane conversion and some selected species concentrations were investigated. The results show that plasma discharging converts methane to hydrogen and heavier hydrocarbons such as C2H3, C2H4,C2H5, C2H6,...
Design and Development of a Turbulent Partially-Premixed Jet Burner
, M.Sc. Thesis Sharif University of Technology ; Salehi, Mohammad Mahdi (Supervisor) ; Mardani, Amir (Co-Supervisor)
Abstract
The burners studied in the combustion principles have different types due to the configuration of different types of flames, each of them studies a specific phenomenon of combustion, so researchers need to design burners with the ability to: create different types of combustion flow regimes, changing in mixing rate and performance at critical points are felt more and more. This document describes the process of designing and manufacturing a turbulent jet burner with variable mixing ratio and the ability to create a diverse range of flow regimes and different flame configurations. Mixing rate is the most important characteristic in the stability of premixed flames, so the distinctive feature...
Optimization of the Eddy Dissipation Concept (EDC) model for turbulence-chemistry interactions under hot diluted combustion of CH4/H2
, Article Fuel ; Volume 191 , 2017 , Pages 114-129 ; 00162361 (ISSN) ; Sharif University of Technology
Elsevier Ltd
2017
Abstract
Moderate or Intense Low-oxygen Dilution (MILD) combustion which known as a combustion under highly preheated and diluted condition is a relatively new combustion regime including many differences in comparison with the traditional one. Among many distinguished disparities between combustion modeling of conventional and MILD ones, turbulent-chemistry interaction modeling is an open field of study. Current knowledge on modeling this combustion regime shows that the eddy dissipation concept (EDC) model could be successfully used for modeling of this combustion regime. In this paper, it has been tried to propose some guidelines to modify the semi-empirical constants of the original EDC model for...
Methylidyne (CH*)Chemiluminescence Measurement in Sooting Flames
, M.Sc. Thesis Sharif University of Technology ; Salehi, Mohammad Mahdi (Supervisor) ; Mardani, Amir (Supervisor)
Abstract
In this study, using a non-interference experimental method, the chemical luminosity of CH* in co-flow diffusion flames with soot and using natural gas hydrocarbon in a laminar flow regime has been investigated. In addition to experimental research, in current research, numerical simulation has been used to extract information such as temperature field, mass fraction of species, and flow structure and comparison and validation with experimental results. Numerical simulation has been used to simulate the mechanism of CH* species formation. Two different mechanisms have been used. In addition, the Soot simulation model from the Moss-Brookes model and radiation heat transfer mechanism...
Essays In Iranian Wholesale Electricity Market
, Ph.D. Dissertation Sharif University of Technology ; Fatemi Ardestani, Farshad (Supervisor) ; Ghazizadeh, Mohammad Sadegh (Supervisor)
Abstract
In this thesis, consider three important questions in the Iranian Wholesale Electricity Market (IWEM) and answer its. The first one is whether the bidding behavior of the firms in the IWEM has been ex-post optimal? The results of the research show that, on average, the firm’s bidding behavior didn’t optimal in the IWEM, and therefore the bidding strategy of them could be improved. This issue is importance from the regulatory viewpoint in terms of assessing market efficiency and market power of firms, as well as from the firm’s point of view to improve the bidding strategy and increase its profits. The second issue is the assessment of the firm’s ability to exercise unilateral market power by...
Application of Micro Combustion In Boundary Layer Control
, M.Sc. Thesis Sharif University of Technology ; Javadi, Khodayar (Supervisor) ; Mardani, Amir (Co-Advisor)
Abstract
The present study focus is on finding a new solution to control laminar separation bubble phenomenon by combustion actuators in micro scale, which is investigated in flows with low Reynolds number surface effect and free flows. The main parameters in this problem are classified in three groups of formation location of laminar separation bubble, its length, and transition from laminar to turbulent around airfoil SD8020 in attack angle of 5 and 8 degree. Following that, the new combustion actuators in micro scale method the comparison it with cold (and hot) air jet injection is introduced to control boundary layer flow with separation bubble point of view. Some mechanisms are identified in...
NO x formation in H 2-CH 4 blended flame under MILD conditions
, Article Combustion Science and Technology ; Volume 184, Issue 7-8 , Aug , 2012 , Pages 995-1010 ; 00102202 (ISSN) ; Tabejamaat, S ; Sharif University of Technology
2012
Abstract
In this article, NO production mechanisms for CH 4-H 2 combustion under MILD (moderate or intense low-oxygen dilution) conditions are studied using CDF and also zero-dimensional well stirred reactor (WSR) analysis. A H 2/CH 4 jet into a heated and diluted coflow is modeled in CFD analysis. The RANS equations with modified k equations are solved in an axisymmetric 2D computational domain. The GRI2.11 full mechanism is considered to represent the chemical reactions. The effects of oxidizer oxygen concentration, fuel hydrogen content, and fuel jet Reynolds number are studied on NO formation reactions. Results show that the measurements are predicted with an acceptable accuracy. The NNH and N 2O...
An accurate guidance algorithm for implementation onboard satellite launch vehicles
, Article Scientia Iranica ; Volume 17, Issue 2 D , JULY-DECEMBE , 2010 , Pages 175-188 ; 10263098 (ISSN) ; Mobed, M ; Sharif University of Technology
2010
Abstract
An algorithm for guiding a launch vehicle carrying a small satellite to a sun synchronous LEO is presented. Before the launch, a nominal path and the corresponding nominal control law for the entire journey are computed. For each sampling instant during the guided flight, a linear equation approximately relating the differences between the actual and nominal values is considered, and a LeastSquares formula using data from on-line state measurements is applied to compute the actual control. The coefficient matrices of the Least-Squares formula can be determined by off-line computations. The method enjoys simplicity of implementation by onboard computers, as well as robust accuracy against...
Numerical study of flame structure in the mild combustion regime
, Article Thermal Science ; Volume 19, Issue 1 , 2015 , Pages 21-34 ; 03549836 (ISSN) ; Tabejamaat, S ; Sharif University of Technology
Serbian Society of Heat Transfer Engineers
2015
Abstract
In this paper, turbulent non-premixed CH4+H2 jet flame issuing into a hot and diluted co-flow air is studied numerically. This flame is under condition of the moderate or intense low-oxygen dilution combustion regime and related to published experimental data. The modelling is carried out using the EDC model to describe turbulence-chemistry interaction. The DRM-22 reduced mechanism and the GRI2.11 full mechanism are used to represent the chemical reactions of H2/methane jet flame. The flame structure for various O2 levels and jet Reynolds numbers are investigated. The results show that the flame entrainment increases by a decrease in O2 concentration at air side or jet Reynolds number. Local...
Numerical investigation of supercritical combustion of H2-O2
, Article Energy and Fuels ; Volume 32, Issue 3 , 2018 , Pages 3851-3868 ; 08870624 (ISSN) ; Barani, E ; Sharif University of Technology
American Chemical Society
2018
Abstract
This study investigates GH2/LOX coaxial jet flame at trans- and supercritical conditions using the Reynolds averaged Navier-Stokes approach. Four two-equation-turbulence models, three real equation of states, two chemical mechanisms, and three different chamber pressures are examined. Predictions show good agreement with measurements qualitatively and quantitatively. Based on the results, the predictions of the Soave-Redlich-Kwong equation of state (EOS) are closer to the experiment, while the Aungier-Redlich-Kwong EOS has more deviation than the others. Moreover, the k-ω shear stress transport model has better performance than the other turbulence models. It is also found that the flow...
Numerical assessment of MILD combustion enhancement through plasma actuator
, Article Energy ; Volume 183 , 2019 , Pages 172-184 ; 03605442 (ISSN) ; Khanehzar, A ; Sharif University of Technology
Elsevier Ltd
2019
Abstract
One promising solution to achieve moderate or intense low-oxygen dilution (MILD) combustion under lower temperatures may be using non-equilibrium plasma discharge. Plasma assisted combustion can extend the flammability limits by reducing the auto-ignition temperature of the reactants and can be a great approach to achieve steady MILD combustion under extreme conditions through decreasing ignition delay time. In particular, the influence of the outlet flows from a co-flowing cylindrical dielectric barrier discharge (DBD) on the CH4/N2 combustion under MILD combustion has been investigated numerically through some simplifications on plasma discharge. A three streams coaxial burner are modeled...