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اطلاعات دوره: 
  • سال: 

    1402
  • دوره: 

    53
  • شماره: 

    4
  • صفحات: 

    291-297
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    44
  • دانلود: 

    5
چکیده: 

In this paper, recommended spiral passive micromixer was designed and simulated. spiral design has the potential to create and strengthen the centrifugal force and the secondary flow. A series of Simulations were carried out to evaluate the effects of channel width, channel depth, the gap between loops, and flowrate on the micromixer performance. These features impact the contact area of the two fluids and ultimately lead to an increment in the quality of the mixture. In this study, for the flow rate of 25 μl/min and molecular diffusion coefficient of 1×10-10 m2/s, mixing efficiency of more than 90% is achieved after 30 (approximately one-third of the total channel length). Finally, the optimized design fabricated using proposed 3D printing method.

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نویسندگان: 

MAO Z. | WU J. | ZHANG L.

نشریه: 

ADVANCES IN WATER SCIENCE

اطلاعات دوره: 
  • سال: 

    2003
  • دوره: 

    14
  • شماره: 

    6
  • صفحات: 

    700-705
تعامل: 
  • استنادات: 

    1
  • بازدید: 

    182
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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بازدید 182

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نویسندگان: 

Rank e. | KRAFCZYK M.

اطلاعات دوره: 
  • سال: 

    2002
  • دوره: 

    3
  • شماره: 

    1
  • صفحات: 

    33-45
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    252
  • دانلود: 

    0
چکیده: 

This paper gives a survey on different types of geometric models being suitable for Numerical Simulation techniques. They are classified in coarse- and fine-grain models for topologically 'rigid' and topologically transient structures. For structural problems, these models are linked to the p-version of the finite element method, and for problems in fluid dynamics, the Lattice Boltzmann method is applied.

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اطلاعات دوره: 
  • سال: 

    2014
  • دوره: 

    13
تعامل: 
  • بازدید: 

    166
  • دانلود: 

    0
چکیده: 

THE CURRENT WORK PRESENTS A Numerical Simulation OF THE INLET BUZZ FOR AN AXISYMMETRIC SUPERSONIC INLET AT FREE STREAM MACH NUMBER OF 2. INLET IS SUBJECTED TO THE DIFFERENT OUTFLOW CONDITIONS. LOW MASS FLOW CONDITIONS LEAD TO THE FLOW INSTABILITY CALLED "BUZZ" IN WHICH THERE ARE TIME-DEPENDENT FLUCTUATIONS IN FLOW FIELD AND INLET SHOCK MOVES FORWARD AND BACKWARD DURING THE BUZZ. THE BUZZ PHENOMENA ARE PREDICTED NumericalLY AND COMPARED BY COMPARING THE EXISTING EXPERIMENTAL RESULTS. THE TIME-DEPENDENT VARIATIONS OF SHOCK LOCATION AND PRESSURE DISTRIBUTION ARE REPORTED.

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نویسندگان: 

PATANKAR N.A. | JOSEPH D.D.

اطلاعات دوره: 
  • سال: 

    2001
  • دوره: 

    27
  • شماره: 

    10
  • صفحات: 

    1685-1706
تعامل: 
  • استنادات: 

    1
  • بازدید: 

    187
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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بازدید 187

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نویسندگان: 

SEDAGHAT A. | MOKHTARIAN S.

اطلاعات دوره: 
  • سال: 

    2013
  • دوره: 

    6
  • شماره: 

    1 (22)
  • صفحات: 

    33-40
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    346
  • دانلود: 

    0
چکیده: 

Rayleigh-Taylor (RT) instability has a growing importance in many fields including aircraft industry and astrophysics. The development and the growth of RT instability were investigated using sinusoidal disturbances with different wavelength at the interface of the two fluids. Numerical Simulations were performed by solving Navier-Stokes unsteady equations with the VOF formulation. Results of the 2D Simulation are compared with experimental results.It is shown that beyond a critical time, not captured experimentally, the mushroom shape of RT instability turns into a helical path or breaks down into a patchy shape depending on the shape of disturbance. Nonlinear instabilities responsible for such behavior are apparent when the wavelength exceeds 10 times the length scale introduced in this study.

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نویسندگان: 

SHEN H.T. | HWANG D.S. | WASANTHA LAL A.M.

اطلاعات دوره: 
  • سال: 

    1995
  • دوره: 

    9
  • شماره: 

    3
  • صفحات: 

    107-118
تعامل: 
  • استنادات: 

    1
  • بازدید: 

    154
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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بازدید 154

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نویسندگان: 

JAFARIAN A. | PISHEVAR A.

اطلاعات دوره: 
  • سال: 

    2016
  • دوره: 

    9
  • شماره: 

    6
  • صفحات: 

    2981-2992
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    279
  • دانلود: 

    0
چکیده: 

In this research, the Supercavitation phenomenon in compressible liquid flows is simulated. The one-fluid method based on a new exact two-phase Riemann solver is used for modeling. The cavitation is considered as an isothermal process and a consistent equation of state with the physical behavior of the water is used. High speed flow of water over a cylinder and a projectile are simulated and the results are compared with the previous Numerical and experimental results. The cavitation bubble profile in both cases agrees well with the previous experimental results reported in the literature. As the result shows, coupling the two-phase Riemann solver with the considered EOS prepares a robust method for simulating the compressible fluid flow with cavitation which can undertake the whole physical behavior of water in a supercavitation process.Furthermore, the influence of the cavitator head and the flow speed on the supercavitation bubble is explored.The results show that cavitators with sharper head results in a smaller supercavitating bubble. Increasing the flow speed beyond a specific limit does not have any significant effect on the cavitation bubble and slightly increases the bubble size.

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اطلاعات دوره: 
  • سال: 

    1395
  • دوره: 

    14
  • شماره: 

    45
  • صفحات: 

    63-78
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    1512
  • دانلود: 

    405
چکیده: 

یکی از ساده ترین وسایلی که برای مکش و پمپ کردن سیال بکار می روند جت اجکتورها هستند. در این تحقیق با استفاده از دینامیک سیالات محاسباتی به شبیه سازی عددی جت اجکتور مادون صوت هوا-هوا پرداخته شده است. معادلات ناویراستوکس، پیوستگی و انرژی با شرایط مرزی بدون لغزش در دیواره حاکم می باشند. شبیه سازی عددی به صورت سه بعدی صورت گرفته و جریان پایا، لزج و مغشوش فرض شده است. به منظور شبیه سازی اغتشاشات از معادلات ناویراستوکس میانگین گیری شده رینولدز K-e Standard، K-e RNG، K- e Realizable، K- w Standard و K-w SST استفاده شده است. ضریب اجکتینگ برای نسبت های فشار متفاوت پارامتر موثری بود که از آن برای صحه گذاری نتایج عددی استفاده گردید. میزان خطا برای مدل توربولانسی K-e RNG کمینه بوده لذا در ادامه، از این مدل به منظور شبیه سازی اغتشاشات استفاده شده است. پس از معتبر سازی نتایج به بررسی پارامتر هندسی تاثیر قطر خروجی دیفیوزر و زاویه واگرایی بر کارآیی جت اجکتور مادون صوت هوا-هوا پرداخته شده است. نتایج نشان می دهد که علاوه بر زاویه واگرایی، قطر خروجی دیفیوزر تاثیر قابل توجهی بر عملکرد و راندمان این نوع دستگاه ها دارد.

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اطلاعات دوره: 
  • سال: 

    2004
  • دوره: 

    2
  • شماره: 

    4
  • صفحات: 

    0-0
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    350
  • دانلود: 

    0
چکیده: 

A two-dimensional Numerical model has been developed to study wave breaking on a sloping beach. The basic elements of Numerical model are Reynolds Averaged Navier-Stokes (RANS) equations that describe the mean flow motion of a turbulent flow; a k turbulence closure model that describes the turbulent transport and dissipation process; an efficient technique (VOF- Volume Of Fluid method) for tracking the free surface motion; and a new scheme developed by Lin and Liu (1999) for wave generation. Shoaling, breaking and overturning of solitary wave on a slope of 1/16 have been studied with the main emphasis on turbulence characteristics. Turbulence characteristics i.e., turbulence kinetic energy, k; turbulence dissipation rate, ; turbulence production, pr; turbulence eddy viscosity, vt; and their spatial distribution during the breaking process have been discussed in great details. Spatial distribution of turbulence characteristics and the order of magnitude have been found to be in agreement with existing experimental and Numerical studies. The main characteristic of plunging breaking waves, the shoreward advective transport of turbulence, has also been investigated and Numerically proved.

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