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Total 114 records

    Multidisciplinary Design Optimization of an Air Launch Satellite Launch Vehicle by Considering the Coupled Slosh–vehicle Dynamics

    , M.Sc. Thesis Sharif University of Technology Keshavarz Mohammadian, Moein (Author) ; Fathi, Mohsen (Supervisor)
    Abstract
    In this thesis, the multidisciplinary design of liquid propellant satellite launch vehicle has been done by taking into consideration the effects of fuel sloshing. At first, the theory of multidisciplinary design and one-level architecture with the label of multidisciplinary feasibility have been used. In the following, Gravitational Search Algorithm (GSA) and Particle swarm optimization (PSO) have been developed. Then, the multidisciplinary design cycle began with the design of the liquid propellant system. In the propulsion section, the selection of the optimal fuel, the design of the nozzle, motor and the selection of the optimal engine cycle considering the geometric and mass... 

    Multidisciplinary Design Optimization of a Nanorobot for Drug Delivery to Cancer Cells Based on Metaheuristic Algorithms

    , M.Sc. Thesis Sharif University of Technology Kazembeigi, Saeideh (Author) ; Abedian, Ali (Supervisor) ; Ghorbanian, Kaveh (Supervisor)
    Abstract
    This thesis is about multidisciplinary design optimization of MRI ¬controlled robots with a nonlinear model approach in the cardiovascular system and simulates its behavior to reach cancer cells. Such robots, designed to perform medical procedures with minimal side effects to the patient, include a set of ferromagnetic nanoparticles attached to the polymer and disposable drugs such as cancer drugs.The disciplines considered in this issue include structure, hydrodynamics, propulsion, controllability, and trajectory. The proposed model in this study, in addition to the main forces acting on the robot such as magnetic force, hydrodynamics, and apparent weight, also examines other forces due to... 

    A Framework for the Optimal and Robust Tolerance Design of Compressor Blades Under Functional Uncertainties”

    , M.Sc. Thesis Sharif University of Technology Mirhosseini, Darya (Author) ; Khodaygan, Saeed (Supervisor)
    Abstract
    Improving the performance of compressors plays a key role in saving energy in industries. The presence of aleatory and epistemic uncertainties, such as dimensional, geometrical and environmental uncertainties, causes the tolerances that are within the allowed ranges in normal assembly conditions to violate the assembly requirements in operational conditions and cause a drop in compressor efficiency. In order to reach the dimensional and geometrical tolerances of the components of a compressor, especially in the design of the rotor and stator blades, that guarantees the optimal and stable performance while not increasi the production costs, there is a need for an optimal and robust tolerance... 

    Modelling and Optimization of Long-Term Heat Storage Systems in Greenhouses

    , M.Sc. Thesis Sharif University of Technology Mohebi, Parastoo (Author) ; Roshandel, Ramin (Supervisor)
    Abstract
    Heating demand required for greenhouses is mainly met by fossil fuels. On the other hand, anxieties over usage of fossil fuels have led the societies to move toward renewable energies. With this in mind, the purpose of this research is to analyze using both solar energy for satisfying the heating demand of greenhouses and heat storage for compensating the intermittence of renewable energy.Considering the mentioned points, in the current research, a linear optimization framework has been developed for design and operation of energy systems including long-term heat storage to meet heating demand of greenhouses. The objective of this framework is to minimize annual cost. The developed method... 

    Reliability-Based Multidisciplinary Design Optimization Under Uncertainty for Reusable Flexible Launch Vehicle Using Genetic Algorithm

    , M.Sc. Thesis Sharif University of Technology Mojibi, Motahareh (Author) ; Fathi Jegarkandi, Mohsen (Supervisor)
    Abstract
    In this research, a Reusable Flexible Launch Vehicle (RFLV) design problem is presented by Multi-Disciplinary Design Optimization (MDO) approach in primary design phase. Trajectory, structure, aerodynamic, aeroelasticity and thermal protection system are considered as involved disciplines in design problem. The study purpose will be to obtain an optimal trajectory which meets all the control and structure limitation while the estimating body skin and thermal protection thicknesses base on structural evaluating in re-entry trajectory is in process. The flexible launch vehicle body is considered as a free-free Bernoulli-Euler beam and D’alembert’s principle addresses inertia force in static... 

    Improving the Decision-Making Process under the Presence of Uncertainty in Airplane Conceptual Design, Creating an Intuitive Platform

    , M.Sc. Thesis Sharif University of Technology Gholinejhad, Nargess (Author) ; Banazadeh, Afshin (Supervisor)
    Abstract
    Improving performance and reducing costs is a constant competition between aircraft designers, which has made multi-disciplinary optimization always part of the design process. In the design process of a conventional aircraft, there are various uncertainties in technology levels, mission parameters, costs and operating environment. It is clear that these uncertainties will make the decision-making difficult and lead to uncertainties in the output of the design; on the other hand, considering them will increase the computational cost. Understanding how much the uncertainty of each parameter will affect the overall output of the design and its performance, makes it possible to ignore the... 

    Conceptual Design of a Solid Propellant Nanolauncher

    , M.Sc. Thesis Sharif University of Technology Ghadiri, Sajjad (Author) ; Farahani, Mohammad (Supervisor) ; Mohammadi, Alireza (Co-Supervisor)
    Abstract
    Nanolaunchers are launch vehicles capable of carring light payloads (under 50 kg) to Low Earth orbit and received much attention in the few past years. Launching the nanosatellites grown about 30 times from 2008 to 2017. Since this category of launch vehicles has fewer developing costs and lower thechnology level, they fit developing space technology in our country. Conversely, the demand of high propellant mass fraction and specific impulse may be a serious difficulty to attain this technology.The only operating nanolauncher in the world is SS-520-5 which belongs to Japan and is a three-stage solid propellant launcher. The goal of this project is also the conceptual design and feasiblity... 

    An Optimized Automated Design Algorithm for Pipeline ADC

    , M.Sc. Thesis Sharif University of Technology Sadrafshari, Mir Vala (Author) ; Sharifkhani, Mohammad (Supervisor)
    Abstract
    Analog to digital converters with different specifications are widely used in modern electronic circuits. The significant demand on pipeline converters in several low power applications is mainly due to their high speed and high resolution characteristics. Fast and simple design of analog circuits using CAD tools, is highly sought after by integrated circuit designers. In this thesis, pipeline analog to digital converters is studied and a CAD tool is proposed for transistor level design and optimizations. The main advantage of this design in comparison with the previous works is that the yield and power consumption are considered as optimization factors. The module operates in three parts:... 

    Multidisciplinary Design Optimization of a Guided Flying Vehicle Considering Uncertainties

    , M.Sc. Thesis Sharif University of Technology Zandavi, Miad (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    Uncertainty-based Multidisciplinary Design Optimization (UMDO) is a growing approach in design of complex engineering which has been of great interest to many design bureau and research center especially in field of aerospace. The UMDO goal is to achieve a global optimum design using effective disciplines, interdisciplinary relations and appropriate uncertainty modeling. In this regard, choosing main analysis, design discipline, uncertainty modeling and their content fitness, formulating the problem structure, interaction of disciplines, modeling level of fidelity and the optimization method are the most important challenge of the MDO problem so UMDO is a new trend of MDO, and have been the... 

    A Novel Approach to Multi Fidelity Multi-objective Conceptual Design Optimization of a Cloud Seeding UAV

    , M.Sc. Thesis Sharif University of Technology Davoodpour, Mostafa (Author) ; Banazade, Afshin (Supervisor)
    Abstract
    In this project, process of conceptual design and design optimization is presented for a cloud seeding UAV. Inefficiency of classical and statical design approaches is more obvious in new designed missions restricted to different and numerous Dynamic and performance constraints with no similar design target aircraft. So in this project we used conceptual design optimization approach with respect to aerodynamic, weight and balance, performance and stability discipline to overcome those restrictions and to design a cloud seeding UAV. In order to reduce the computational time, we used low fidelity method (analectic equation) in performance and stability, medium fidelity method (empherical... 

    Reliability-based Multidisciplinary Design Optimization of an Aeroelastic Projectile

    , M.Sc. Thesis Sharif University of Technology Khodabakhsh, Amir Hossein (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    In this research, Reliability-Based Multidisciplinary Design Optimization has been addressed. For this purpose, the main concepts in reliability-based design are investigated and the design methods based on reliability are explained. Providing a unified formulation to implement the optimal design structure based on the reliability, is the second part of this research. It has been intended to present a suitable structure for the design process considering the existing formulas and considering the numerical solutions. An aeroelastic projectile has been chosen as the target system for implementing the proposed process in the present study. The third section of this document has been dedicated... 

    A Framework for Lifetime Management and Optimization of Hybrid Renewable Energy System Based on Integrated Methodology of Design and Energy Management System (Operation). Case study: Integrated Photovoltaic/wind Turbine System

    , Ph.D. Dissertation Sharif University of Technology Behzadi Forough, Atefeh (Author) ; Roshandel, Ramin (Supervisor)
    Abstract
    In this project, a comprehensive methodology is developed to present the lifetime management and optimization framework for hybrid renewable energy systems. The main purpose of this work is to minimize the lifetime cost and improve the system reliability based on the interaction between different optimization levels related to different steps in the system lifetime. The proposed methodology is generally presented by providing a connection between the three specified optimization levels: 1) Planning: including design and long-term optimization models which is performed before system operation, 2) Real-time operation: By employing the receding horizon optimization which is applied from the... 

    Turbine blade aerodynamic optimization on unstructured grids using a continuous adjoint method

    , Article ASME 2012 International Mechanical Engineering Congress and Exposition, IMECE 2012, Houston, TX, 9 November 2012 through 15 November 2012 ; Volume 1 , 2012 , Pages 425-431 ; 9780791845172 (ISBN) Zeinalpour, M ; Mazaheri, K ; Irannejad, A ; Sharif University of Technology
    2012
    Abstract
    A gradient based optimization using the continuous adjoint method for inverse design of a turbine blade cascade is presented. The advantage of the adjoint method is that the objective function gradients can be evaluated by solving the adjoint equations with coefficients depending on the flow variables. This method is particularly suitable for aerodynamic design optimization for which the number of design variables is large. Bezier polynomials are used to parameterize suction side of the turbine blade. The numerical convective fluxes of both flow and adjoint equations are computed by using a Roe-type approximate Riemann solver. An approximate linearization is applied to simplify the... 

    Multidisciplinary design of a guided flying vehicle using simplex nondominated sorting genetic algorithm II

    , Article Structural and Multidisciplinary Optimization ; Volume 57, Issue 2 , February , 2018 , Pages 705-720 ; 1615147X (ISSN) Zandavi, S. M ; Pourtakdoust, S. H ; Sharif University of Technology
    Springer Verlag  2018
    Abstract
    This paper presents design of a typical Guided Flying Vehicle (GFV) using the multidisciplinary design optimization (MDO). The main objectives of this multi-disciplinary design are maximizing the payload’s weight as well as minimizing the miss distance. The main disciplines considered for this design include aerodynamics, dynamic, guidance, control, structure, weight and balance. This design of GFV is applied to three and six Degree of Freedom (DOF) to show comparison of simulation results. The hybrid scheme of optimization algorithm is based on Nelder-Mead Simplex optimization algorithm and Nondominated Sorting Genetic Algorithm II (NSGA II), called Simplex-NSGA II. This scheme is... 

    Use of response surface methodology analysis for xanthan biopolymer production by xanthomonas campestris: focus on agitation rate, carbon source, and temperature

    , Article Iranian Journal of Chemistry and Chemical Engineering ; Volume 36, Issue 1 , 2017 , Pages 173-183 ; 10219986 (ISSN) Zakeri, A ; Pazouki, M ; Vossoughi, M ; Sharif University of Technology
    Jihad Danishgahi  2017
    Abstract
    The current study is an attempt to contribute for efficient and cost-effective substrates for xanthan gum production. In this context, the sugar cane molasses wastes can be used as a cheap substrate for xanthan gum production. Xanthan biopolymer production by a novel Xanthomonas campestris strain IBRC-M 10644 was optimized with statistical approaches. Based on the results of Response Surface Methodology (RSM) with Central Composite Design (CCD) technique, a second-order polynomial model was developed and evaluated the effects of variables on the maximum xanthan production. Agitation rate (X1: 200-500 rpm), sugar cane molasses concentration (X2: 30-90 g/L) and operation temperature (X3: 25-35... 

    Performance optimization of the helical heat exchanger with turbulator

    , Article Frontiers in Energy Research ; Volume 9 , 2022 ; 2296598X (ISSN) Xifeng, W ; Xiaoluan, Z ; Mahariq, I ; Salem, M ; Ghalandari, M ; Ghadak, F ; Abedini, M ; Sharif University of Technology
    Frontiers Media S.A  2022
    Abstract
    In this paper, optimization on a two-tube helical heat exchanger with a fin is represented. The spiral pipes heat exchanger which is made of the cooper is adopted for investigation. The effects of three types of fins with the proposed geometric shapes on the overall heat transfer coefficient and pressure loss are investigated. The fins are located on the inner surface of the outer pipe. The obtained numerical results are compared with the experimental results, and a good agreement is observed between the results. The studies show that the total heat transfer coefficient has increased by 170% compared to an exchanger with no fin. Therefore, the best fin has been selected based on the... 

    Design, analysis, and implementation of extra low air-gap single-phase axial-flux induction motors for low-cost applications

    , Article International Transactions on Electrical Energy Systems ; Volume 26, Issue 12 , 2016 , Pages 2516-2531 ; 20507038 (ISSN) Tootoonchian, F ; Nasiri Gheidari, Z ; Lesani, H ; Sharif University of Technology
    John Wiley and Sons Ltd 
    Abstract
    In this paper, design and prototyping of two-speed capacitor-run single-phase axial-flux induction motor (AFIM) for direct-drive applications is presented. The proposed structure has single stator-single rotor configuration with high magnetic pull between the stator and rotor, which may compel rotor to lock. Although the most efficient method to overcome this problem is using a second rotor or stator in the mirror with the first one, it is not applicable in low-cost applications. So, in this paper, two new and fast construction techniques are proposed to fabricate an AFIM with extra low air-gap length and minimum cost. Beside design and optimization process, a thermal equivalent circuit... 

    Optimal riser design in sand casting process with evolutionary topology optimization

    , Article Structural and Multidisciplinary Optimization ; Volume 38, Issue 2 , 2009 , Pages 205-214 ; 1615147X (ISSN) Tavakoli, R ; Davami, P ; Sharif University of Technology
    2009
    Abstract
    The optimal design of a casting feeding system is considered. The riser topology is systematically modified to minimize the riser volume, while simultaneously ensuring that no defect appears in the product. In this approach, we combine finite-difference analysis of the solidification process with evolutionary topology optimization to systematically improve the feeding system design. The outstanding features of the presented method are: its efficiency, ease of implementation and simplifying definition of the initial design. The efficiency and capability of the presented method are supported by illustrative examples. © 2008 Springer-Verlag  

    Optimal riser design in sand casting process by topology optimization with SIMP method I: poisson approximation of nonlinear heat transfer equation

    , Article Structural and Multidisciplinary Optimization ; Volume 36, Issue 2 , 25 January , 2008 , Pages 193-202 ; 1615147X (ISSN) Tavakoli, R ; Davami, P ; Sharif University of Technology
    2008
    Abstract
    The optimal design of a casting feeding system is considered. The problem is formulated as the volume constrained topology optimization and is solved with the finite element analysis, explicit design sensitivity, and numerical optimization. In contrast to the traditional topology optimization where the objective function is defined on the design space, in the presented method, the design space is a subset of the complement of the objective function space. To accelerate optimization procedure, the nonlinear unsteady heat transfer equation is approximated with a Poisson-like equation. The feasibility of the presented method is supported with illustrative examples. © 2007 Springer-Verlag  

    Optimization of composite patch repair for inclined crack on aluminum plate using genetic algorithm

    , Article 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, 25 September 2016 through 30 September 2016 ; 2016 ; 9783932182853 (ISBN) Talebi, B ; Abedian, A ; Firooz, S ; Sharif University of Technology
    International Council of the Aeronautical Sciences  2016
    Abstract
    In this study, a composite patch repair will be designed for an aluminum plate with a central crack placed at 45 degrees to the applied unidirectional tensile load carried by the plate. In this state, the condition of loading is mixed mode. In the first step, behavior of the crack repaired by the composite patch under the applied tensile load is simulated by using ABAQUS commercial software. The crack growth process is modeled with the extended finite element method (XFEM) and the cohesive zone model (CZM) is used to model any damage progression in the adhesive of the composite patch repair. The shape of the five layer composite patch is assumed to be elliptical. For design optimization, the...