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    An experimental study of time lag for pressure measurement in different tubes

    , Article Amirkabir (Journal of Science and Technology) ; Volume 16, Issue 61 B , 2005 , Pages 127-137 ; 10150951 (ISSN) Mani, M ; Soltani, M. R ; Tolouei, E ; Sharif University of Technology
    2005
    Abstract
    Determination of the time lag caused by utilization of different tubes to measure pressure on the surface of a wind tunnel model is an important problem in the field of aerodynamic especially for unsteady measurements where the pressure signature changes continuously with time. In this investigation the time required for the applied pressure at one end of different tubes to reach its original value (applied pressure) at the other end has been measured. Three plastic tubes and two polyethylene tubes with different lengths and different inner diameters; L=2, 5 and 10 m, d=1, 2 and 4 mm, were used to study the time lag. Experimental data show that the response time in a pressure measuring... 

    Experimental flow visulization of single swirl spray pattern at various pressure drops

    , Article 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, 20 July 2003 through 23 July 2003 ; 2003 ; 9781624100987 (ISBN) Ghorbanian, K ; Ashjaee, M ; Soltani, M. R ; Mesbahi, M. H ; Morad, M. R ; Sharif University of Technology
    2003
    Abstract
    An experimental investigation of the flow field of pressure swirl atomizers for different pressure drops is performed. Two experimental methods are employed. For low injection pressures, a visual study is conducted while for higher pressures the velocity components and size of the droplets are measured by using Phase Doppler Anemometer. The spray formation, spray cone angle, and breakup length are visually investigated. Velocity and size of the droplets are measured on a plane of measurement along the axis of the spray so that the properties are carried out in a radial direction as a function of both pressure drop and axial distance from the nozzle. Self-similar mean axial velocity profiles... 

    Neural network analysis of single swirl spray pattern at various pressure drops

    , Article 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, 20 July 2003 through 23 July 2003 ; 2003 ; 9781624100987 (ISBN) Soltani, M. R ; Ghorbanian, K ; Ashjaee, M ; Morad, M. R ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2003
    Abstract
    Radial Basis Function, a neural network based interpolation method, is used to simulate swirling spray phenomenon. From this model, the profile of mean velocity components' distribution along the main axis of the injector at various pressure drops and spray measurements' plane are obtained and analyzed. Experimental data obtained through Phase Doppler Anemometer is used to train this model. The results are compared with experimental data as well as to those obtained through General Regression Neural Network method as another neural network based interpolation method investigated previously by the authors. © 2003 by M.R. Soltani  

    Effect of plunging amplitude on the performance of a wind turbine blade section

    , Article Aeronautical Journal ; Volume 111, Issue 1123 , 2007 , Pages 571-588 ; 00019240 (ISSN) Soltani, M. R ; Marzabadi, F. R ; Sharif University of Technology
    Royal Aeronautical Society  2007
    Abstract
    Extensive low speed wind-tunnel tests were conducted to study the unsteady aerodynamic behaviour of an airfoil sinusoidally oscillating in plunge. The experiments involved measuring the surface pressure distribution over a range of amplitudes, H = ±5 to ±15cm. In addition, steady state data were acquired and were used to furnish a baseline for further analysis and comparison. The model was oscillated with a constant reduced frequency, k = 0.058, at three mean angles of attack of 0°, 10° and 18°. The unsteady aerodynamic loads were calculated from the surface pressure measurements, 64 ports, along the chord for both upper and lower surfaces of the model. The plunging displacements were... 

    Experimental results of pressure variation in two-phase air-water flow in water tunnels

    , Article 31st IAHR Congress 2005: Water Engineering for the Future, Choices and Challenges, 11 September 2005 through 16 September 2005 ; 2005 , Pages 6523-6533 ; 8987898245 (ISBN); 9788987898247 (ISBN) Kabiri Samani, A ; Byong-Ho J ; Sang I. L ; Won S. I ; Gye-Woon C ; Sharif University of Technology
    Korea Water Resources Association  2005
    Abstract
    An experimental investigation has been carried out to verify characteristics of pressure fluctuations inside a circular, horizontal and inclined pipeline (90mm inside diameter and 10 m long) carrying two-phase air-water flow in a controlled manner (operating at room temperature and normal pressure). The pressure fluctuation was considered to be due to interaction between the fluid and air bubble compressibility in the pipe. The fluctuating pressure was studied in detail while the flow pattern was mainly slug, wavy or stratified flow. The tests were carried out varying with time, space, water flow rate/air flow rate ratio and pipe inclination. The pressure fluctuations were measured... 

    Jet impact geometry and plunge pool dimensions effects on dynamic pressures at pool sidewalls

    , Article Canadian Journal of Civil Engineering ; Volume 35, Issue 4 , 2008 , Pages 408-417 ; 03151468 (ISSN) Borghei, S.M ; Zarnani, P ; Sharif University of Technology
    2008
    Abstract
    A plunge pool is one of the energy dissipater structures for high head dams, which ensures stability of the dam under extreme hydrodynamic pressure, due to falling jet impacts. The excess energy of the jet is dissipated, together with significant impact pressure exerted on the floor and pool walls. Thus, appropriate assessment of jet dynamic characteristics in the plunge pool is essential. This research presents experimental results focusing on. the distribution of mean and extreme pressure fluctuations on the sidewalls, due to circular and rectangular plunging jets, and the effects of pool dimension, especially in narrow valleys. The experimental variables are discharge, geometry of jet,... 

    Non-steady burning effect on solid rocket motor performance

    , Article 45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, 8 January 2007 through 11 January 2007 ; Volume 14 , 2007 , Pages 9531-9536 ; 1563478900 (ISBN); 9781563478901 (ISBN) Tahsini, A. M ; Sharif University of Technology
    American Institute of Aeronautics and Astronautics Inc  2007
    Abstract
    Solid rocket performance during rapid pressure excursions differs greatly from predictions based on steady state burning rate data. Rapid pressurization following a chamber filling interval produces indicated burning rate overshoots. Transient internal ballistics of a solid propellant rocket motor during rapid pressurization part of chamber filling phase has been considered in this work. Quasi one-dimensional unsteady Euler equations with a transient propellant burning model that accounts for the effects of time rate of change of the chamber pressure on the burning rate have been used to simulate the internal ballistics of rocket motors. The compressible convective flow solver used in this... 

    On the effects of aero boundary layer control on pressure drag reduction in supercavitating bodies

    , Article 24th International Conference on Offshore Mechanics and Arctic Engineering, 2005, Halkidiki, 12 June 2005 through 17 June 2005 ; Volume 2 , 2005 , Pages 665-675 Khakpour, Y ; Yazdani, M ; Sharif University of Technology
    2005
    Abstract
    Supercavitation is known as the way of viscous drag reduction for the projectiles, moving in the liquid phase. In recent works, there is distinct investigation between cavitation flow and momentum transfer far away from the cavity surface. However, it seems that there is strong connection between overall flow and what takes place in the sheet cavity where a constant pressure distribution is assumed. Furthermore as we'll see, pressure distribution on cavity surface caused due to overall conditions, induct nonaxisymetric forces and they may need to be investigated. Primarily we describe how pressure distribution into the cavity can cause separation of the aero boundary layer. Then we present... 

    Numerical study of diodicity mechanism in different tesla-type microvalves

    , Article Journal of Applied Research and Technology ; Volume 11, Issue 6 , 2013 , Pages 876-885 ; 16656423 (ISSN) Nobakht, A. Y ; Shahsavan, M ; Paykani, A ; Sharif University of Technology
    2013
    Abstract
    Microvalve is one of the most important components in microfluidic systems and micropumps. In this paper, threedimensional incompressible flow through a Tesla-type microvalve is simulated using FLUENT computational fluid dynamic package. The flow is laminar and SIMPLE algorithm is used. The second-order upwind method is implemented for discretizing convective terms. The diodicity mechanism is investigated in detail for three different microvalves. Effect of several series Tesla-type microvalves on diodicity is also studied. The numerical analyses reveal that the mechanism of diodicity occurs at the T-junction and side channel. If inlet and outlet channels are eliminated, diodicity can be... 

    Complexity of density dependencies of thermal and internal pressure compared to that of total pressure

    , Article Industrial and Engineering Chemistry Research ; Volume 52, Issue 23 , May , 2013 , Pages 8034-8045 ; 08885885 (ISSN) Sajjadi, S . H ; Parsafar, G ; Sharif University of Technology
    2013
    Abstract
    A simple equation of state (EoS) has recently been introduced (J. Phys. Chem. B2009, 113, 11977-11987) as (Z - 1)v2 = e + f/ρ + gρ2, where Z ≡ pv/RT is the compressibility factor, v = 1/ρ is molar volume, and e, f, and g are temperature dependent parameters. This EoS has been found to be accurate for all types of nano and bulk solids and bulk fluids, in the entire temperature and pressure ranges for which experimental data are reported, except for the isotherms within 1 ≤ T r = T/Tc ≤ 1.1 for the spherical and near spherical species and for a wider temperature range for the cylindrical molecules. The aim of this work is to investigate the validity of a three-term expression similar to the... 

    Developing a new pressure measurement mechanism based on squeeze film damping effect

    , Article Proceedings - 2011 2nd International Conference on Control, Instrumentation and Automation, ICCIA 2011, 27 December 2011 through 29 December 2011 ; Dec , 2012 , Pages 800-803 ; ISBN: 9781467316897 Ghafari, A ; Ghanbari, A ; Kamanzadeh, S ; Abbasian, K ; Saghir, H ; Sharif University of Technology
    IEEE Computer Society  2012
    Abstract
    This paper introduces a novel approach for measuring low pressures based on MEMS technology. In this technique the mechanism of squeeze film damping is used. A voltage is applied to a fixed-fixed MEMS beam and its step response is obtained; for each pressure there is a different response. Then the settling time is measured and we can relate each settling time with a defined pressure. Here, first we use some equations to relate pressure with the squeeze film damping effect; after that we use a micro beam model and relate its parameters with pressure. Then we use numerical analysis and simulation to show the procedure of pressure measuring. All simulation results are shown and discussed  

    Computational investigation of graphene behavior under differential water pressure and possible mass transfer influences

    , Article ASME 2016 5th International Conference on Micro/Nanoscale Heat and Mass Transfer, MNHMT 2016, 4 January 2016 through 6 January 2016 ; Volume 2 , 2016 ; 9780791849668 (ISBN) Jafari, S ; Darbandi, M ; Saidi, M.S ; Heat Transfer Division ; Sharif University of Technology
    American Society of Mechanical Engineers  2016
    Abstract
    Because of its unique properties, graphene has attracted the attentions of many academic research groups and recently, the industry. One of the promising applications of the graphene is in micro/nano-sensors, e.g. using it as a pressure sensor. To use it in mechanical-based nano-sensors, it is very important to investigate the mechanical behavior of the nano-sized graphene sheet and its sensitivity to the medium changes applied on its faces. In this work, we use the molecular dynamics MD method and simulate the behavior of graphene sheet under differential water pressure influences. In this regard, a square straight monolayer graphene sheet is placed as a separator diaphragm between two... 

    Condensate blockage study in gas condensate reservoir

    , Article Journal of Natural Gas Science and Engineering ; Volume 33 , 2016 , Pages 634-643 ; 18755100 (ISSN) Rahimzadeh, A ; Bazargan, M ; Darvishi, R ; Mohammadi, A. H ; Sharif University of Technology
    Elsevier  2016
    Abstract
    The effect of condensate blockage on the pressure drop near the well bore has been studied. Two types of single well simulations have been conducted and pressure drop due to condensate blockage has been quantified based on variation of gas relative permeabilities in near well bore area. The relationship of condensate banking pressure drop, gas rate and reservoir quality has been presented. It is shown that for a poor reservoir quality, condensate blockage can increase the pressure drop up to 200% of the pressure drop in the tubing  

    Evaluation of water impact for symmetric wedge by experimental and numerical methods

    , Article International Journal of Applied Mechanics and Engineering ; Volume 24, Issue 1 , 2019 , Pages 221-230 ; 17344492 (ISSN) Nikfarjam, M ; Koto, J ; Yaakob, O. B ; Seif, M. S ; Aref, A ; Sharif University of Technology
    Sciendo  2019
    Abstract
    Evaluation of impact loads when a ship hull contacts the wave surface is one of the main issues for researchers who are going to design the structure of marine vehicles. In this paper, the results of experimental tests and numerical modeling of the distribution of pressure on different wedge-shaped models are reported and the effect of related parameters such as the deadrise angles, the weight and drop heights, is assessed. The output of analyses and the results can give appropriate approximations of the maximum impact pressures for the geometries that are similar to marine vehicle's hull sections to estimate the hydrodynamic impact loads in different sea-states. In addition, other effective... 

    Pressure leaching of chalcopyrite concentrate with oxygen and kinetic study on the process in sulfuric acid solution

    , Article Transactions of the Indian Institute of Metals ; Volume 73, Issue 4 , 6 March , 2020 , Pages 975-987 Mojtahedi, B ; Rasouli, S ; Yoozbashizadeh, H ; Sharif University of Technology
    Springer  2020
    Abstract
    In this research work, the pressure leaching of chalcopyrite concentrate with oxygen was studied. Experiments were carried out under conditions of the solid–liquid ratio of 0.1, agitation speed of 750 rpm, and sulfuric acid concentration of 2 M in a stainless-steel autoclave system under 0.6 to 1 MPa oxygen gas. Central composite design was used to design experiments, and three factors of temperature, time, and oxygen pressure were selected as the design variables. A linear model for %Cu and a quadratic model for %Fe were proposed by Minitab Software. The results showed that temperature is the most effective factor in chalcopyrite leaching. Under optimal conditions, 93.08% of copper with the... 

    Structural and electronic properties of YBa2Cu3O7 under high pressures

    , Article Physica C: Superconductivity and its Applications ; Volume 370, Issue 2 , 2002 , Pages 85-93 ; 09214534 (ISSN) Khosroabadi, H ; Mohammadi Zadeh, M. R ; Akhavan, M ; Sharif University of Technology
    2002
    Abstract
    The structural and electronic properties of YBa2Cu3O7 have been investigated by the total energy-pseudopotential method within the local density approximation. We have calculated the charge density, length of bonds, band structure and density of states for ambient and high pressures, and the change of hole concentration with pressure in this system. Our results show increase of holes in both CuO2 planes and Cu-O chains under high pressures. Bulk modulus and equilibrium volume have also been calculated to be equal 184 GPa and 174.89 Å3, respectively. © 2001 Elsevier Science B.V. All rights reserved  

    Charge density distribution with pressure in Y-123

    , Article Physica B: Condensed Matter ; Volume 321, Issue 1-4 , 2002 , Pages 360-364 ; 09214526 (ISSN) Khosroabadi, H ; Mohammadi Zadeh, M. R ; Akhavan, M ; Sharif University of Technology
    2002
    Abstract
    The structural and electronic properties of YBa2Cu3O7 have been investigated by the total energy-pseudopotential method within the local density approximation. We have calculated charge density and length of bonds for ambient and high pressures, and the change of hole concentration with pressure in this system. Our results show the increase of holes in both CuO2 planes and Cu-O chains under high pressures. Bulk modulus and equilibrium volume have been also calculated to be 184 GPa and 174.89 Å3, respectively. © 2002 Elsevier Science B.V. All rights reserved  

    Experimental and simulation investigation of pulsed heat pipes in gas compressors

    , Article AIMS Energy ; Volume 8, Issue 3 , 2020 , Pages 438-454 Alizadeh, A ; Shafii, M. B ; Mirzahosseini, A. H ; Ataei, A ; Sharif University of Technology
    AIMS Press  2020
    Abstract
    In natural gas pressure boosting stations, air coolers are used to reduce the gas temperature. Pressure drop as an essential factor in determining the energy performance of any pressure boosting station has a significant impact on the overall performance of the gas transmission. In this paper, a laboratory pilot is designed to investigate the effect of pressure drop reduction on the use of heating pipes at the air coolers. In addition, as a case for a gas pressure boosting station, its impact over energy performance index and pressure drop parameter has been calculated through simulating. The results show, implemented PHP tubes in an air cooler, lead to reduce tube length and improve... 

    Fractal analysis of asphaltene aggregation phenomena in live oils at elevated pressure and temperature

    , Article Particulate Science and Technology ; Volume 38, Issue 4 , 2020 , Pages 454-463 Mohammadi, S ; Rashidi, F ; Mousavi Dehghani, S. A ; Ghazanfari, M. H ; Sharif University of Technology
    Taylor and Francis Inc  2020
    Abstract
    In this work, high-pressure microscopy technique was used to measure the size and fractal dimension of asphaltene aggregates formed in different live oil samples at elevated pressures and temperatures. It was found that the asphaltene aggregates in live oil samples are irregular fractal-like structures with pressure−temperature-dependent fractal dimensions. By monitoring the variation of the fractal dimension and size of the asphaltene aggregates with pressure and temperature, the mechanisms responsible for asphaltene aggregation process at elevated pressures and temperatures can be well predicted. The range of fractal dimension of asphaltene aggregates in live oils is similar to that... 

    Experimental investigation of velocity profiles in the wake of an oscillating airfoil

    , Article 2007 5th Joint ASME/JSME Fluids Engineering Summer Conference, FEDSM 2007, San Diego, CA, 30 July 2007 through 2 August 2007 ; Volume 1 SYMPOSIA, Issue PART B , August , 2007 , Pages 1873-1882 ; 0791842886 (ISBN); 9780791842881 (ISBN) Soltani, M. R ; Mahmoudi, M ; Sharif University of Technology
    2007
    Abstract
    A series of experiments were carried out to study the unsteady wakes behind an oscillating airfoil. The airfoil is a section of a wind turbine blade oscillating in pitch about the quarter chord axis at various reduced frequencies, oscillation amplitude and mean angles of attack. Real time velocity profiles were obtained using total and static pressure at 35 vertically aligned points behind the airfoil via two similar rakes. The rakes were located at a distance of 1.5 chord length behind the model. The results show great influence of oscillation amplitude and reduced frequency on the wake velocity profiles. Copyright © 2007 by ASME