computational study
در نشریات گروه فنی و مهندسی-
The paper investigates the aerodynamic performance and power requirement characteristics of wing sections integrated with high-lift airfoil to support the operation of solar-powered Unmanned Aerial vehicle (UAV). The flight mission is aimed to simulate the operation of solar-powered UAVs under low -speed environment. The research focuses on studying the aerodynamic effect of non-solar UAV wing model and solar UAV wing model for the varying angle of attack. The UAV wing models are tested using a subsonic wind tunnel to validate the aerodynamic characteristics at low-speed condition. The aerodynamic parameters such as coefficient of lift (Cl), coefficient of drag (Cd), coefficient of pressure (Cp), and the total power required to accelerate the solar UAV are studied to maintain steady level flight. The solar UAV and non-solar UAV wing models were subjected to a computational process to examine the pressure and velocity distributions for the aerodynamic performance analysis. Evident results show that the solar cells positioned at the flow separation region of the UAV wing model produces an aerodynamic efficiency rate of 5.45% and required 37.13W of minimum power compared to non-solar UAV at the Reynolds number of 9.8 106.Keywords: Aerodynamics drag, Computational Study, Solar cell, Unmanned aerial vehicle, Wind tunnel
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دندان به عنوان یکی از اعضای مهم بدن، در زیبایی نقش اساسی داشته و یکی از بهترین راه ها برای درمان نامرتبی و خرابی آن تا به امروز، استفاده از ارتودنسی می باشد. سیم های ارتودنسی هوشمند به جهت مرتب کردن دندان و بدلایلی نظیر رفتار ابرکشسانی، مقاومت در برابرخوردگی، عمرخستگی بالا، سازگاری خوب با دهان و کرنش برگشت پذیر کاربرد بسیاری دارند. در این مقاله از روش اجزاء محدود جهت بررسی رفتار مکانیکی سیم های ارتودنسی هوشمند مطابق استاندارد با اعمال نیروی کششی و با در نظرگرفتن خواص متالورژیکی آنها استفاده شد. مدل ماکروسکوپی جهت توصیف خواص ماده بر اساس انرژی آزاد ترمودینامیکی هلمهولتز بود. نتایج نشان داد: با تغییر10 درجه ای دمای کلینیکی از 26 تا 36 درجه سانتیگراد، تنش های مسطح بالایی و پایینی و انرژی الاستیک ذخیر شده به ترتیب حدود10و 28/18درصد کاهش یافتند. همچنین با تغییر10درجه ای دمای کلینیکی از 36 تا 46 درجه سانتیگراد، به ترتیب تنش های مسطح بالایی و پایینی و انرژی الاستیک ذخیر شده حدود 18و 26/47درصد افزایش یافتند. در نهایت سیم ارتودنسی هوشمند با سطح اختلاف تنش های مسطح بالایی و پایینی کمتر ، انرژی کرنش الاستیک پایین تر، حلقه هیسترزیس وابسته به رفتار ابرکشسانی کامل تر و تطابق بالای نتایج تجربی و عددی مربوط به تغییرات نیرو-کرنش، عملکرد بهتری نشان داد. این مطالعه عددی میتواند یک روشی برای بررسی رفتار مکانیکی سیم های ارتودنسی هوشمند با توجه به اثرات خواص متالورژیکی و مکانیکی جهت اثر بخشی طول درمان در دندان ارایه نماید.
کلید واژگان: دندان، سیم های ارتودنسی هوشمند، خواص مواد، بررسی محاسباتیTeeth, as one of the most important organs of the body, play an essential role in beauty and one of the best ways to treat its disorder and damage to date is the use of orthodontics. Smart wires are widely used in orthodontics for tidying teeth and for reasons such as superelastic behavior, corrosion resistance, high fatigue life, good compatibility and reversible strain. In this paper, the finite element method was used to investigate the mechanical behavior of smart orthodontic wires according to the standard by applying tensile force and considering their metallurgical properties. The macroscopic model for describing the properties of matter was based on Helmholtz thermodynamic free energy. The results showed that: With a 10°C changes in clinical temperature from 26°C to 36°C, the upper and lower plateau stresses and the strain elastic energy decreased about 10% and 18.28% respectively. Also with 10°C change in clinical temperature from 36°C to 46°C, the upper and lower plateau stresses and the strain elastic energy increased approximately 18% and 47.26% respectively. In conclusion, the smart orthodontic wire due to the lower level of the difference between the upper and lower plateau stresses, less elastic strain energy, hysteresis loop and complete dependent on superelastic behavior and high correlation of experimental and numerical results related to force-strain changes showed better performance. This numerical study can provide a method to study the mechanical behavior of smart orthodontic wires with respect to the effects of metallurgical and mechanical properties for the effectiveness of the length of treatment in the tooth.
Keywords: Computational study, material properties, smart, Orthodontic Wire, Teeth -
استنت های از جنس آلیاژحافظه دار نایتینولی می تواند بدلیل کاهش دادن مشکلاتی نظیر رفتار دینامیکی نامناسب، قابلیت پیچ خوردن کم و استحکام شعاعی ناکافی سایر استنت ها برای استفاده در نای بکار رود. در این مقاله از روش اجزاء محدود برای بررسی رفتار مکانیکی و کلینیکی استنت های از جنس آلیاژحافظه دار نایتینولی برای کاربرد در نای انسانی استفاده شد. ارزیابی استنت ها با اعمال کرنش شعاعی مطابق استاندارد و با در نظرگرفتن خواص متالورژیکی و مکانیکی آنها انجام گرفت. مدل ماده مورد استفاده جهت توصیف خواص ماده حافظه داربر اساس انرژی ترمودینامیکی آزاد هلمهولتز (مدل آریشیو) و انرژی ترمودینامیکی آزاد گیبس (مدل لاگوداس) بود. استنت از جنس آلیاژحافظه دار نایتینولی با خواص ماده دارای دمای آستنیتی 24 درجه سانتیگراد بدلایلی نظیر نیروی مناسب اعمالی به مجرا، استحکام مقاومتی شعاعی مطلوب و حلقه هیسترزیس کامل وابسته به رفتار ابرکشسانی بعلاوه تنش کمتر و کرنش بیشتر عملکرد مکانیکی و کلینیکی بهتری نشان داد.
کلید واژگان: استنت حافظه دار، مطالعه محاسباتی، نای، دمای پایان آستنیتیJournal of Iranian Metallurgical and Materials Engineering Society, Volume:24 Issue: 82, 2022, PP 87 -97Simulation of Nitinol shape memory alloy stents behavior for application in trachea stent implantation has been strategically used for solving trachea stenosis. Predicaments like insufficient radial strength, low twisting ability, inappropriate dynamic behavior and restenosis are expected to be solved by the introduction of new designs. Superelastic shape memory alloy stent is an interesting alternative for minimizing these tight spots. The application of finite element method to predict metallurgical of superelastic shape memory alloy stents for trachea duct dilatation is supported by conventional crimp tests. The present simulation modeled the stent material’s superelasticity based on Auricchio theories (Helmholtz free energy) and Lagoudas (Gibbs free energy).Nitinol shape memory alloy stents with material properties contain Af temperature of 24°C° is shown to have the best mechanical performance for clinical applications. Owing to lower chronic outward force (COF), higher radial resistive force (RRF), and more suitable superelastic behavior. Model calculations showed that a very high change of Af temperature could exert a substantial effect on practical performance of the stent. This FEM model can provide a convenient way for evaluation of biomechanical properties of peripheral stents given to effects of metallurgical properties such as austenite finish temperature.
Keywords: Computational study, Austenite Finish Temperature, Shape memory alloy Stents, Trachea lumen -
Wind energy is one of the abundantly available renewable energy resources. Savonius vertical axis wind turbine is better suited for small scale power generation applications with many advantages. The turbine operates independent of wind direction with good starting torque and less noise. But, the power coefficient of the Savonius turbine is less than all other wind turbines. The shape of the turbine blades plays an important role in the performance of the turbine. In this present two-dimensional numerical study, an attempt has been made to improve the turbine performance by considering three types of blade shapes. The complete design details of the proposed new blade shapes are presented. The simulations are carried out using ANSYS Fluent 15.0 with SST K-ω turbulence model. The power coefficient of the modified blade is found to have increased by 20% compared to conventional blade shape. The effect of tip-speed-ratio on power coefficient has also been studied and reported.Keywords: Computational Study, Savonius turbine, Wind turbine, Power coefficient, Blade shape, Performance improvement
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A detailed numerical investigation of two different modes of shock wave-turbulent boundary layer interaction (SWBLI) is presented. Equivalence of ramp induced SWBLI (R-SWBLI), and impingement shock based SWBLI (I-SWBLI) is explored from the computational study using an in-house developed compressible flow solver. Multiple flow deflection angles and ramp angles are employed for this study. For all the investigated cases, a freestream Mach number of 2.96 and Reynolds number of 3.47×107m−1 are considered. The k−ε model with the improved wall function of present solver predicted wall pressure distributions and separation bubble sizes very close to the experimental measurements. However, the separation bubble size is slightly over overpredicted by the k−ω model in most of the cases. The effect of overall flow deflection angle and upstream boundary layer thickness on the SWBLI phenomenon is also studied. A nearly linear variation in separation bubble size is observed with changes in overall flow deflection angle and upstream boundary layer thickness. However, the equivalence of SWBLI is noted to be independent of these two parameters. The undisturbed boundary thickness at the beginning of the interaction is identified as the most adequate scaling parameter for the length of the separated region.
Keywords: Shock waves, Computational study, SWBLI-Equivalence, Turbulence modelling, Finite VolumeMethod, Boundary layer, Flow separation -
Natural or industrial flows of a fluid often involve droplets or bubbles of another fluid, pinned by physical or chemical impurities or by the roughness of the bounding walls. Here we study numerically one drop pinned on a circular hydrophilic patch, on an oscillating incline whose angle is proportional to sin(ωt). The resulting deformation of the drop is measured by the displacement of its center of mass, which behaves similarly to a driven over-damped linear oscillator with amplitude A(ω) and phase lag φ(ω). The phase lag is O(ω) at small ω like a linear oscillator, but the amplitude is O(ω−1) in a wide range of large ω instead of O(ω−2) for a linear oscillator. A heuristic explanation is given for this behaviour. The simulations were performed with the software Comsol in mode Laminar Two-Phase Flow, Level Set, with fluid 1 as engine oil and fluid 2 as water.Keywords: Droplet, Pinning, Two-Phase flow, Driven oscillator, Finite elements, Computational study
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