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    Flight Dynamic Modeling of an Articulated FMAV Using Quasi Steady Aerodynamics

    , M.Sc. Thesis Sharif University of Technology Ghashghaei, Arash (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    This thesis is focused on flight dynamics modeling and analysis of an articulated Flapping Micro Air Vehicle (FMAV), where the articulating joint is placed near the wing mid chord span. The articulation modeling, its results and verification due to added degrees of freedom are considered the key motivation and novelties of this project. Initial analyses indicated that a simple articulation device such as joint is not appropriate and will not be efficient for flying FMAV. As a corrective action, a spring-damper mechanism was utilized beside the articulation. Subsequently, the kinematics’ equations are developed and verified using the MSC Automated Dynamic Analysis of Mechanical Systems... 

    Evaluation of quasi-steady aerodynamic modeling for flutter prediction of aircraft wings in incompressible flow

    , Article Thin-Walled Structures ; Volume 44, Issue 9 , 2006 , Pages 931-936 ; 02638231 (ISSN) Haddadpour, H ; Dehghani Firouz Abadi, R ; Sharif University of Technology
    2006
    Abstract
    In this paper, the aeroelastic behavior and flutter instability of aircraft wings in subsonic incompressible flight speed regime are investigated. Quasi-steady and unsteady aerodynamic models are used for aerodynamic modeling and the obtained aeroelastic predictions are compared to those available in the specialized literature. Based on a number of test cases, it is shown that the quasi-steady aerodynamic models are inadequate for the determination of aeroelastic behavior and flutter boundary of aircraft wings in the incompressible flight speed range. © 2006 Elsevier Ltd. All rights reserved  

    Numerical simulation of three-dimensional flow and analysis of filling process in compression resin transfer moulding

    , Article Composites Part A: Applied Science and Manufacturing ; Volume 37, Issue 9 , 2006 , Pages 1434-1450 ; 1359835X (ISSN) Shojaei, A ; Sharif University of Technology
    2006
    Abstract
    In compression resin transfer moulding (CRTM), resin flows inside a mould filled with fibrous reinforcement as a result of resin injection and mould compression. This process facilitates the resin flow through the fibrous reinforcement particularly for high fiber content parts. This paper presents the numerical simulation of filling process of CRTM in full three-dimensional domain. A mathematical model of three-dimensional resin flow inside the CRTM mould is presented. An effective elastic modulus is introduced for multi-layer preforms connecting the mould closing speed to deformation rate of individual layers. Control volume/finite element method (CV/FEM) is used and the numerical algorithm... 

    Aeroelastic Modeling, Experimental Validation and Stability Analysis of a Flapping Wing Air Vehicle in Planar Flight

    , Ph.D. Dissertation Sharif University of Technology Karimian Aliabdi, Saeed (Author) ; Pourtakdoust, Hossein (Supervisor)
    Abstract
    In this research, aeroelastic model of an elastic flapping wing has been derived in order to be integrated with the flight dynamic model. The model developed in this research well describes the coupled and nonlinear behavior of the passive torsional deformations of the wing during flapping motion. Based on this obtained equations, a precise propulsion model proper for flapping wing vehicles has been introduced. The effect of geometric and mechanical properties of the wing is being accounted. In order to validation of the analytical model several FMAVs as well as an instrumented test stand for online measurements of forces, flapping angle and power consumption have been designed and built... 

    Control of Cable Vibration under Rain-wind Induced Vibration with Magneto-rheologycal Jacketing

    , M.Sc. Thesis Sharif University of Technology Turkesh, Purya (Author) ; Haddadpour, Hassan (Supervisor)
    Abstract
    The present thesis follows two aims in the phenomenon of vibration and control of cable of cable-stayed bridge under rain-wind induced vibration (RWIV). The first one is to study the response of the cable and consequently the second one aims to control these vibrations that occurred in the cable. The assumed continuous cable has lateral, in plane bending (IP), out of plane bending (OOP) and torsion mode. The effect of rainfall on the cable has been modeled with mobile upper rivulet on the cable surface and the effect and shape of lower rivulet have been neglected. RWIV is not vortex-induced vibration (VIV), nor wake galloping, because the dominant frequency of RWIV is lower than VIV and... 

    Aeroelastic Analysis of Flying Wing Aircrafts

    , M.Sc. Thesis Sharif University of Technology Joulaei, Mohammad Moin (Author) ; Dehghan Firouzabadi, Rouhollah (Supervisor) ; Haddadpour, Hassan (Supervisor)
    Abstract
    Purpose of this thesis is to discover the governing equation of Flying Wing aircrafts. In Flying Wing aircrafts crew, payload, fuel, and equipment are typically housed inside the main wing structure. A clean flying wing is sometimes presented as theoretically the most aerodynamically efficient (lowest drag) design configuration for a fixed wing aircraft. We assume Flying wing as plate. Achieve structural formulation needs to use modal deflections and put them in Lagrangian equations. In the right had side, pressure on flying wing can be found. To obtain air pressure on flying wing in this thesis, applying Quasi steady aerodynamic and Howe distribution is necessary. Applying this method on ... 

    Modeling and Simulation of a Dragonfly-like Micro Aerial Vehicle with Rigid Wings

    , M.Sc. Thesis Sharif University of Technology Toulabi, Sobhan (Author) ; Banazadeh, Afshin (Supervisor)
    Abstract
    Dynamical behavior of a dragonfly-like with rigid flapping wings considering aerodynamic forces has been modelled and simulated. At first, the dragonfly with its unique flying capabilities and the reasons for choosing it has been introduced. Then, modelling process is started with preliminary definitions including frames, coordinates and equations of motion, continued by applying initial conditions and ended with verification tests. After that, aerodynamic effects in a quasi-steady sense is added to dynamical model resulting in an 18 DOF model developed to be used for nonlinear simulation or controller designing. At the end, the results are validated in comparison to an experimental study.... 

    A modified solar desalination system using evacuated tube collector

    , Article Desalination ; Volume 396 , 2016 , Pages 30-38 ; 00119164 (ISSN) Shafii, M. B ; Jahangiri Mamouri, S ; Lotfi, M. M ; Jafari Mosleh, H ; Sharif University of Technology
    Elsevier  2016
    Abstract
    Solar energy is turning to one of the important types of clean energies, due to its availability, and its potential for wide range of applications. In this work, a new passive solar desalination system is introduced, which benefits from excellences of twin-glass evacuated tube collectors. For the first time, the evacuated tube collector is not only used as the solar thermal collector, but also as a basin to heat the water. Hence, the thermal resistance between the collector and basin is virtually eliminated. Results show a considerable increase in the rate of desalinated water production and the maximum production reaches up to 0.83 kg/(m2·h). It was observed that the maximum rate of the... 

    Aero-thermoelastic stability of functionally graded plates

    , Article Composite Structures ; Volume 80, Issue 4 , 2007 , Pages 580-587 ; 02638223 (ISSN) Navazi, H. M ; Haddadpour, H ; Sharif University of Technology
    2007
    Abstract
    In this paper, an analytical investigation intended to determine the aero-thermoelastic stability margins of functionally graded panels is carried out. For this purpose, piston theory aerodynamics has been employed to model quasi-steady aerodynamic loading. The material properties of the plate are assumed to be graded continuously across the panel thickness. A simple power-law and the Mori-Tanaka scheme are used for estimating the effective material properties such as temperature-dependent thermoelastic properties. The effects of compressive in-plane loads and both uniform and through the thickness non-linear temperature distributions are also considered. Hamilton's principle is used to... 

    Effects of slip condition on the characteristic of flow in ice melting process

    , Article International Journal of Engineering, Transactions B: Applications ; Volume 18, Issue 3 , 2005 , Pages 253-261 ; 1728-144X (ISSN) Raoufpanah, A ; Rad, M ; Borujerdi, A. N ; Sharif University of Technology
    Materials and Energy Research Center  2005
    Abstract
    In this paper a laminar flow of water on an ice layer subjected to a slip condition is considered numerically. The paper describes a parametric mathematical model to simulate the coupled heat and mass transfer events occurring in moving boundary problems associated with a quasi steady state steady flow process. The discretization technique of the elliptic governing differential equations of mass, momentum and energy is based on the control volume finite difference approach and enthalpy method, the results illustrate, the distribution of heat transfer coefficient, ice melting thickness, slip velocity at solid moving boundary and boundary layer thickness for some values of slip velocity... 

    Development of Transient Model of Fuel Consumption to Optimize IVT

    , M.Sc. Thesis Sharif University of Technology Ebadi, Mohammad (Author) ; Saadat Foumani, Mahmoud (Supervisor) ; Kazemzade Hannani, Siamak (Co-Advisor)
    Abstract
    Changes in the internal structure of engines for reducing fuel consumption has almost stopped. While changes in powertrain is a better way to reduce vehicle fuel consumption. Recently, infinitely variable transmissions or IVTs have attracted large attention of car manufacturers . In these systems, due to the continuous transmission ratio, engine speed is kept in a range which is the optimum fuel consumption speed range. Designing of these systems for each vehicle must be done according to the requirements of the vehicle and engine abilities. So, an exact model of engine fuel consumption for the design of these systems is required. One way of improving the accuracy of conventional models, is... 

    Implementation of Time Splitting Projection Method in water hammer modeling in deformable pipes

    , Article International Journal of Pressure Vessels and Piping ; Volume 98 , October , 2012 , Pages 30-42 ; 03080161 (ISSN) Niroomandi, A ; Borghei, S. M ; Bohluly, A ; Sharif University of Technology
    Elsevier  2012
    Abstract
    In this paper Time Splitting Projection Method (TSPM) has been implemented to model transient flow in a deformable pipe. In addition a quasi-steady model and the Brunone unsteady model have been incorporated into the algorithm to consider the effect of static and dynamic friction on the shape and attenuation of pressure waves. The deformation of the cross section of the pipe due to the change of pressure has been considered using Hooke's Law of elasticity. Numerical results of the model have been compared with a simple analytical test and results of experimental measurements for water hammer problem with different Reynolds numbers in a simple pipeline system; besides, numerical stability... 

    Numerical study of random lasing in three dimensional amplifying disordered media

    , Article Optics Communications ; Volume 285, Issue 6 , 2012 , Pages 1314-1322 ; 00304018 (ISSN) Ghasempour Ardakani, A ; Bahrampour, A. R ; Mahdavi, S. M ; Golshani Gharyeh Ali, M ; Sharif University of Technology
    2012
    Abstract
    In this paper, the lasing action in three-dimensional active random systems has been numerically investigated. Here, random systems of spherical dielectric particles imbedded in an active medium are considered. The quasi steady state approximation for the population inversion of the active medium is applied to solve three dimensional governing equations. Results show that when the density of particles increases to an upper limit, the intensity of lasing modes is enhanced. Also, the effects of pumping rate and particle size on the number of lasing modes and their intensity are studied. Lasing threshold of laser modes in different disordered systems is calculated and it is shown that by an... 

    Oxidation behavior of AISI 321, AISI 316, and AISI 409 stainless steels: Kinetic, thermodynamic, and diffusion studies

    , Article Journal of Materials Research ; 2016 , Pages 1-9 ; 08842914 Movahedi Rad, A ; Pelaseyed, S.S ; Attarian, M ; Shokrallahzadeh, R ; Sharif University of Technology
    Cambridge University Press  2016
    Abstract
    The oxidation behavior of three types of stainless steels, namely AISI 321, AISI 316, and AISI 409, was compared. In all stainless steels, oxide layers were formed and their masses and thicknesses increased with oxidation time. Among them, AISI 409 ferritic stainless steel demonstrated higher oxidation rate. According to the kinetical oxidation behavior of them at elevated temperatures, the oxidation mechanism was determined. Among them, the AISI 409 ferritic stainless steel showed the lowest and AISI 321 austenitic stainless steel demonstrated the highest oxidation resistance. Based on the experimental results, it was suggested that the kinetic of oxide growth in stainless steels was... 

    Evaluation of a transient borehole heat exchanger model in dynamic simulation of a ground source heat pump system

    , Article Energy ; Volume 147 , March , 2018 , Pages 81-93 ; 03605442 (ISSN) Biglarian, H ; Abbaspour, M ; Saidi, M. H ; Sharif University of Technology
    Elsevier Ltd  2018
    Abstract
    The performance of a vertical ground source heat pump system (GSHPS) largely depends on the fluid temperature leaving the borehole heat exchanger (BHE) that may be affected by the short-term behavior of the BHE. Although considerable research has been carried out to analyze the short-term transient response of the BHEs, few studies have investigated its impact on dynamic simulation of GSHPS. Therefore, this paper presents a numerical approach based on a transient BHE model to evaluate the performance of a residential GSHPS over short and long timescales. The numerical results are compared with the results of EnergyPlus software. It is shown that the proposed model can appropriately predict... 

    On the power-bandwidth trade-off in bistable photonic switches

    , Article Photonic and Phononic Crystal Materials and Devices IX, San Jose, CA, 27 January 2009 through 29 January 2009 ; Volume 7223 , 2009 ; 0277786X (ISSN) Naqavi, A ; Abediasl, H ; Mehrany, K ; Khorasani, S ; Chamanzar, M. R ; Adibi, A ; Sharif University of Technology
    2009
    Abstract
    Low power operation and high speed have always been desirable in applications such as data processing and telecommunications. While achieving these two goals simultaneously, however, one encounters the well-known powerbandwidth trade-off. This is here discussed in a typical bistable switch based on a two-dimensional photonic crystal with Kerr type nonlinearity. The discussion is supported by the nonlinear finite difference time domain (FDTD) simulation of a direct coupled structure with a home-developed code. Two cases of working near resonant and off- resonant are simulated to compare the power and the speed of the device in the two cases. It is shown that working nearresonance reduces the... 

    Multi-objective robust design optimization (MORDO) of an aeroelastic high-aspect-ratio wing

    , Article Journal of the Brazilian Society of Mechanical Sciences and Engineering ; Volume 42, Issue 11 , 2020 Elyasi, M ; Roudbari, A ; Hajipourzadeh, P ; Sharif University of Technology
    Springer Science and Business Media Deutschland GmbH  2020
    Abstract
    In this paper, a new approach for multi-objective robust optimization of flutter velocity and maximum displacement of the wing tip are investigated. The wing is under the influence of bending–torsion coupling and its design variables have different levels of uncertainty. In designing and optimizing wings with a high aspect ratio, the optimization process can be done in such a way to increase the flutter velocity, but this can increase the amplitude of the wing tip displacement to a point that leads to the wings damage and structural failure. Therefore, single-objective design optimization may lead to infeasible designs. Thus, for multi-objective optimization, modeling is based on the... 

    A year-round study of a photovoltaic thermal system integrated with phase change material in Shanghai using transient model

    , Article Energy Conversion and Management ; Volume 210 , 2020 Kazemian, A ; Salari, A ; Ma, T ; Sharif University of Technology
    Elsevier Ltd  2020
    Abstract
    In the study, the daily and monthly performance of a photovoltaic thermal system integrated with phase change material is investigated in Shanghai, China. A three-dimensional model of photovoltaic thermal system integrated with phase change material system is developed and numerically simulated. Water is considered as working fluid, and the fluid flow regime is laminar and incompressible. Both quasi-steady and transient models are compared together, and the transient model is selected because of its higher accuracy. Validation analysis is performed on the numerical model to show the reasonable agreement of current research compared to some other research. After obtaining the suitable... 

    Theoretical and experimental study of microstructures and weld pool geometry during GTAW of 304 stainless steel

    , Article International Journal of Advanced Manufacturing Technology ; Volume 42, Issue 11-12 , 2009 , Pages 1043-1051 ; 02683768 (ISSN) Jamshidi Aval, H ; Farzadi, A ; Serajzadeh, S ; Kokabi, A. H ; Sharif University of Technology
    2009
    Abstract
    In this work, temperature field and weld pool geometry during gas tungsten arc welding of 304 stainless steel are predicted by solving the governing equations of heat transfer and fluid flow under quasi-steady state conditions. The model is based on numerical solution of the equations of conservation of mass, momentum, and energy in the weld pool. Weld pool geometry, weld thermal cycles, and various solidification parameters are then calculated by means of the model predictions. The model considers the effects of various process parameters including welding speed and heat input. It is found that the weld pool geometry, predicted by the proposed model, is in reasonable agreement with the... 

    Robust flutter analysis and control of a wing

    , Article Aircraft Engineering and Aerospace Technology ; Volume 84, Issue 6 , 2012 , Pages 423-438 ; 00022667 (ISSN) Fatehi, M ; Moghaddam, M ; Rahim, M ; Sharif University of Technology
    2012
    Abstract
    Purpose - The purpose of this paper is to present a novel approach in aeroservoelastic analysis and robust control of a wing section with two control surfaces in leading-edge and trailing-edge. The method demonstrates how the number of model uncertainties can affect the flutter margin. Design/methodology/approach - The proposed method effectively incorporates the structural model of a wing section with two degrees of freedom of pitch and plunge with two control surfaces on trailing and leading edges. A quasi-steady aerodynamics assumption is made for the aerodynamic modeling. Basically, perturbations are considered for the dynamic pressure models and uncertainty parameters are associated...