به جمع مشترکان مگیران بپیوندید!

تنها با پرداخت 70 هزارتومان حق اشتراک سالانه به متن مقالات دسترسی داشته باشید و 100 مقاله را بدون هزینه دیگری دریافت کنید.

برای پرداخت حق اشتراک اگر عضو هستید وارد شوید در غیر این صورت حساب کاربری جدید ایجاد کنید

عضویت

جستجوی مقالات مرتبط با کلیدواژه « suction » در نشریات گروه « برق »

تکرار جستجوی کلیدواژه «suction» در نشریات گروه «فنی و مهندسی»
  • A. Shakiba, A. Baradaran Rahimi *
    In recent decades, reverse flow analysis in mixed convection flow has attracted the attention of many researchers owing to its applications in the design of medical and engineering systems. The presence of reverse flow is unfavorable in many respects; therefore, it is crucial to find values of critical parameters affecting the reverse flow to eliminate it. In this paper, the thermal and hydrodynamic behavior of MWCNT-Fe3O4 hybrid nanofluid is explored in a vertical cylindrical annulus and in the adjacency of radial magnetic field by achieving the results of the exact solution. Furthermore, the effective factors on the reverse flow are investigated, considering the effects of wall movement and suction/injection on it. The range of changes of the governing parameters includes constant velocity of cylinders’ walls A=0−10, B=0−10, Mixed convection parameter η=-1500−1500, dimensionless temperature difference ratio ξ=0−1, Hartman number Ha=0−50, Suction/injection S=-6−6, nanocomposite particles concentration φ=0−0.3% and radios ratio λ=2−10. The results reveal that hybrid nanofluid enhances the heat transfer rate. Moreover, by changing the above-mentioned parameters and selecting the appropriate values for them, the flow, heat transfer and occurrence of reverse flow can be optimally controlled. Meanwhile, such parameters as Ha, S and ξ perform better in eliminating reverse flow.
    Keywords: Reverse flow, Vertical cylindrical annulus, Hybrid nanofluid, Moving walls, Magnetohydrodynamics (MHD), Mixed convection heat transfer, suction, injection, exact solution}
  • S. Qojevand *, G. Habibagahi, M. Veiskarami
    An extension of the slip line theory to unsaturated soils is presented and applied to the problem of stability of slopes in unsaturated soils. The matric suction is then introduced and implemented in governing equations by the well-known Bishop effective stress concept. In this regard, the van Genuchten model is utilized to estimate the effective stress parameter required for the computation of the effective stress. The influence of the soil matric suction on the stability of slopes has been investigated for a variety of soils under steady state evaporation and infiltration, i.e., the distribution of the matric suction was assumed to remain constant with time. In addition, a measure of stability in terms of some factor of stability has been introduced.
    Keywords: unsaturated soil, slip lines, Slope stability, Suction, van Genuchten Model}
  • F. Jafarzadeh, A. Ahmadinezhad *, H. Sadeghi

    Soil deposits may experience different hydraulic states in terms of suction (ψ) and degree of saturation (Sr) while subjected to large strain caused by dynamic loading during earthquakes. This phenomenon is investigated by considering the effects of initial ψ, initial Sr, sample preparation method, drainage condition, and cycle number (N) on dynamic properties. Shear modulus (G) and damping ratio (D) are specifically studied for an unsaturated sand using a modified cyclic simple shear device for all zones of soil water retention curve (SWRC). Results revealed the relative significance of both ψ and Sr in relation to SWRC on observed trends in G and D. Through analyzing some results from the literature, it was shown that most of the data follow a sigmoid function in the plane of normalized stiffness (G/Gsat) versus suction normalized to the air entry value. It was also revealed that minimum damping is not in conjugation with maximum stiffness due to the contribution of other mechanisms in damping like inter-particle water lubrication. Comparison between results of two testing methods indicated a notable influence of initial fabric on G. Furthermore, the overall trends in G and D against N are marginally influenced by initial ψ and Sr.

    Keywords: Cyclic Simple Shear, Suction, Degree of saturation, shear modulus, damping ratio, Unsaturated Sand}
  • S. Eswaramoorthi, S. Sivasankaran *, S. Rajan, Ali Saleh Alshomrani, M. Bhuvaneswari
    The effects of viscous dissipation and convective boundary condition on the two-dimensional convective flow of a second grade liquid over a stretchable surface with suction/injection and heat generation are investigated. The governing partial differential equations are reduced into a dimensionless coupled system of nonlinear ordinary differential equations by appropriate similarity transformation. Then, they are solved analyticallyby homotopy analysis method (HAM) and by numerically with fourth order Runge-Kutta method with shooting technique. The HAM and numerical results of the local skin friction and local Nusselt number are compared for various emerging parameters. It is found that the momentum boundary layer thickness grows with rising the values of the viscoelastic parameter.
    Keywords: second grade fluid, convective boundary, heat generation, suction, injection, viscous dissipation}
  • پوریا اکبرزاده *، مهسا مصطفوی
    یکی از رویکردهای موثر در بهبود عملکرد آیرودینامیکی هیدروفویل ها و ایرفویل ها، تزریق مقدار اندکی انرژی به سیستم (نظیر تزریق یا مکش سیال روی سطح جسم) ، جهت تغییر نیروی برآ و پسا می باشد. در حقیقت مکش و دمش سطحی سیال می تواند توزیع فشار و گرادیان سرعت روی سطوح ایرفویل/ هیدروفویل را بهبود و محل جدایش جریان را اصلاح نماید. از این رو در تحقیق حاضر به بررسی رفتار هیدرودینامیکی جریان آشفته عبوری از یک ایرفویل که در معرض تزریق و مکش جریان سیال در قسمتی از سطح بالایی خود قرار گرفته است پرداخته می شود. رفتار ایرفویل ابتدا تحت یک موقعیت تزریق یا مکش سیال بررسی و پس از آن تزریق یا مکش از دو موقعیت، مورد بررسی قرار می گیرد. در این شبیه سازی از نرم افزار تجاری فلوئنت بهره گرفته شده است. هدف از این تحقیق، مطالعه اثر قدرت، تعداد شکاف تزریق یا مکش، محل تزریق یا مکش سیال و زاویه تزریق یا مکش روی عملکرد هیدرودینامیکی ایرفویل می باشد. از مهم ترین نتایج به دست آمده می توان به کاهش 10 الی 50 درصدی نیروی پسا و افزایش 5 الی 10 درصدی نیروی برآ (در حالت دمش) و کاهش 5 الی 30 درصدی نیروی پسا و افزایش 5 الی 10 درصدی نیروی برآ (در حالت مکش) با درنظر گرفتن دو شکاف تزریق در مقایسه با یک شکاف تزریق کاهش اشاره کرد.
    کلید واژگان: کنترل جریان, دمش و مکش سیال, ضریب برآ, ضریب پسا, زاویه تزریق جریان}
    Pooria Akbarzadeh *, Mahsa Mostafavi
    One approach to improve the aerodynamic performance of airfoils and hydrofoils is inject a small amount of energy to the system (such as fluid injection or suction on the surface), to change the lift and drag. In fact, surface suction and blowing of the fluid can improve the pressure distribution and velocity gradient on the airfoil/hydrofoil surfaces and modify the flow separation point. Therefore, in this study the hydrodynamic behavior of turbulent flows over an airfoil exposed to the injection and suction of fluid in a part of its upper surface is discussed. Firstly, the behavior of the airfoil under one position of the injection or suction and then under two positions of injection or suction are investigated. In this simulation, the FLUENT software is used. The aim of this study is to investigate the effect of the power, the number, the position and the angle of blowing or suction on the hydrodynamic performance of the airfoil. The most important results are the reduction of 10 to 50 percent of the drag and the increase of 5 to 10 percent of the lift (for the blowing) and the reduction of 5 to 30 percent of the drag and the increase of 5 to 10 percent of the lift (for the suction) by considering two positions of injection in comparison to one position.
    Keywords: Flow Control, Blowing, amp, Suction, Lift Coefficient, Drag Coefficient, Flow Injection Angle}
  • Karim Mazaheri, Ashkan Nejati, Kiarash Charlang Kiani
    Shock Control Bump (SCB) reduces the wave drag in transonic flight. In high Mach transonic flows, the boundary layer separation downstream the bump, induced by the shock wave, results in the poor performance of the SCB. To control the boundary layer separation and to reduce the wave drag for two transonic airfoils, RAE-2822 and NACA-64A010, we investigate the application of two conventional flow control methods, i.e. suction and blowing, to be added to the SCB. An adjoint gradient based optimization algorithm is used to find the optimum shape and location of SCB. The performance of both hybrid suction/SCB (HSS) and hybrid blowing/SCB (HBS) is a function of the sucked or injected mass flow rate, and their position. A parametric study is performed to find the near optimum values of the aerodynamic coefficients and efficiency. A RANS solver is validated and used for this flow analysis. This study shows that both HSS and HBS methods considerably improve the aerodynamic efficiency (L/D), while the HBS method is more effective in control of the shock wave/boundary layer interaction. Using HSS method, the aerodynamic efficiencies of these two airfoils are increased by, respectively, 8.6% and 3.9%, respect to the airfoils with optimized bumps. For HBS configuration, improvements are respectively 13.5% and 9.0%. The best non-dimensional mass flow rate for suction is found to be around 0.003 for both airfoils, and for blowing this is about 0.0025 for RAE-2822 airfoil and about 0.002 for NACA-64A010. The best location for suction and blowing are found to be, respectively, right before and after the SCB.
    Keywords: Transonic airfoil, Shock wave, Drag reduction, Shock Control Bump, Suction, Blowing, Adjoint optimization, Hybrid flow control tools}
  • A. Lashkari
    Based on the concept of independent stress state variables to consider the impact of unsaturated conditions, an elasto-plastic critical state constitutive model for saturated and unsaturated interfaces is introduced in this paper. The proposed model is capable of predicting many characteristics of unsaturated interface behavior, such as the dependence of initial tangent modulus, peak shear stress, dilatancy, and ultimate strength on matric suction, net normal stress, and the interface state measured with respect to the critical state line. To this aim, two distinct yield mechanisms are employed in the model. While change in stress ratio generates plastic deformation in the first mechanism, plastic deformations are due to an increase in net normal stress, decrease in matric suction, or both, in the second mechanism. The presence of appropriate state dependent ingredients enables the model to provide realistic predictions over a wide range of variations of density, net normal stress, and matric suction. By direct comparison of the model predictions with experimental data, the predictive capacity of the proposed model is evaluated.
    Keywords: Constitutive model, Suction, Net normal stress, Interface, Critical state}
نکته
  • نتایج بر اساس تاریخ انتشار مرتب شده‌اند.
  • کلیدواژه مورد نظر شما تنها در فیلد کلیدواژگان مقالات جستجو شده‌است. به منظور حذف نتایج غیر مرتبط، جستجو تنها در مقالات مجلاتی انجام شده که با مجله ماخذ هم موضوع هستند.
  • در صورتی که می‌خواهید جستجو را در همه موضوعات و با شرایط دیگر تکرار کنید به صفحه جستجوی پیشرفته مجلات مراجعه کنید.
درخواست پشتیبانی - گزارش اشکال