scholarly journals The non-Darcy characteristics of fault water inrush in karst tunnel based on flow state conversion theory

2021 ◽  
Vol 25 (6 Part B) ◽  
pp. 4415-4421
Author(s):  
Zheng-Zheng Cao ◽  
Yu-Feng Xue ◽  
Hao Wang ◽  
Jia-Rui Chen ◽  
Yu-Lou Ren
Keyword(s):  
Flow Velocity ◽  
Water Inrush ◽  
Coupled Model ◽  
Flow Fields ◽  
Darcy Law ◽  
Brinkman Equation ◽  
Flow State ◽  
Navier Stokes Equation ◽  
Velocity Change ◽  
Key Factor

The fault water inrush is a key factor which leads to tunnel construction in karst regions. Based on the fluid mechanics principles, the paper addresses a numer?ical coupled model for karst fault tunnel with COMSOL Multiphysics software. Besides, the Darcy law equation, Brinkman equation, and Navier-Stokes equation are inserted to stimulate the steady flow of aquifer, the non-linear seepage of fault and the free flow in tunnel excavating area in software, respectively. Then, the pres?sure and flow velocity in three flow fields are analyzed under different permeability ratios in numerical model. It is shown that the fault permeability is the key factor affecting water inrush, and that the pressure and flow velocity change visibly in adjacent domains between two flow fields.

The Research on the Key Factor Affect the Precision in Stress Analysis for the Rotor of Steam Turbine

2013 ◽  
Vol 275-277 ◽  
pp. 83-86
Author(s):  
Chun Lin Zhang ◽  
Nian Su Hu ◽  
Wen Yang ◽  
Jian Mei Wang ◽  
Min Li ◽  
...  
Keyword(s):  
Heat Transfer ◽  
Heat Transfer Coefficient ◽  
Numerical Calculation ◽  
Transfer Coefficient ◽  
Stress Analysis ◽  
Surface Heat ◽  
Flow State ◽  
Surface Heat Transfer ◽  
Surface Heat Transfer Coefficient ◽  
Key Factor

With the development of the power grid, the proportion of large capacity unit is increasing rapidly. It requires a more in-depth study on the reliability of the unit, especially for the unit adjusting the peak. This paper concerned on the research of the surface heat transfer coefficient, which is the key factor affect the precision in thermal stress analysis. The surface heat transfer coefficient is obtained via the numerical calculation for the steam’s flow state and the transient heat transfer between rotor. This paper mainly describes the steam’s flow state and the transient heat transfer with the steam seal, and the results show that the direct numerical calculation is resultful in this subject.

Numerical Analysis of Flow Fields and Temperature Fields in a Regenerative Heating Furnace for Steel Pipes

2018 ◽  
Vol 10 (3) ◽  
Author(s):  
Yi Han ◽  
Feng Liu ◽  
Xin Ran
Keyword(s):  
Temperature Field ◽  
Flow Field ◽  
Flow Velocity ◽  
Gas Flow ◽  
Flow Fields ◽  
Heating Furnace ◽  
Temperature Fields ◽  
Turbulent Layer ◽  
Steel Pipes ◽  
Pipe Blanks

In the production process of large-diameter seamless steel pipes, the blank heating quality before roll piercing has an important effect on whether subsequently conforming piping is produced. Obtaining accurate pipe blank heating temperature fields is the basis for establishing and optimizing a seamless pipe heating schedule. In this paper, the thermal process in a regenerative heating furnace was studied using fluent software, and the distribution laws of the flow field in the furnace and of the temperature field around the pipe blanks were obtained and verified experimentally. The heating furnace for pipe blanks was analyzed from multiple perspectives, including overall flow field, flow fields at different cross sections, and overall temperature field. It was found that the changeover process of the regenerative heating furnace caused the temperature in the upper part of the furnace to fluctuate. Under the pipe blanks, the gas flow was relatively thin, and the flow velocity was relatively low, facilitating the formation of a viscous turbulent layer and thereby inhibiting heat exchange around the pipe blanks. The mutual interference between the gas flow from burners and the return gas from the furnace tail flue led to different flow velocity directions at different positions, and such interference was relatively evident in the middle part of the furnace. A temperature “layering” phenomenon occurred between the upper and lower parts of the pipe blanks. The study in this paper has some significant usefulness for in-depth exploration of the characteristics of regenerative heating furnaces for steel pipes.

Numerical Simulation of Muzzle Flow Field of Gun Based on CFD

2013 ◽  
Vol 291-294 ◽  
pp. 1981-1984
Author(s):  
Zhang Xia Guo ◽  
Yu Tian Pan ◽  
Yong Cun Wang ◽  
Hai Yan Zhang
Keyword(s):  
Numerical Simulation ◽  
Flow Field ◽  
Stokes Equation ◽  
Wave Structure ◽  
Flow Fields ◽  
Single Equation ◽  
Navier Stokes ◽  
Turbulent Model ◽  
Navier Stokes Equation ◽  
Numerical Simulation Result

Gunpowder was released in an instant when the pill fly out of the shell during the firing, and then formed a complicated flow fields about the muzzle when the gas expanded sharply. Using the 2 d axisymmetric Navier-Stokes equation combined with single equation turbulent model to conduct the numerical simulation of the process of gunpowder gass evacuating out of the shell without muzzle regardless of the pill’s movement. The numerical simulation result was identical with the experimental. Then simulated the evacuating process of gunpowder gass of an artillery with muzzle brake. The result showed complicated wave structure of the flow fields with the muzzle brake and analysed the influence of muzzle brake to the gass flow field distribution.

Pulmonary microcirculatory response to localized hypercapnia

1982 ◽  
Vol 53 (6) ◽  
pp. 1556-1564 ◽  
Author(s):  
T. Koyama ◽  
M. Horimoto
Keyword(s):  
Flow Velocity ◽  
Time Course ◽  
Capillary Flow ◽  
Mean Flow ◽  
Velocity Change ◽  
Luminal Diameter ◽  
Initial Values ◽  
Pulmonary Capillary ◽  
Before And After ◽  
Pulmonary Microvessels

Anesthetized bullfrogs were examined to study the effects of localized hypercapnia on the red blood cell (RBC) velocity in pulmonary alveolar microvessels on the exposed lung surface. Before and after the exposure of a small area of the lung surface 6 mm in diameter to a hypercapnic gas mixture, the region was exposed to CO2-free control gas. The RBC velocity was measured by the use of a laser Doppler microscope. Both mean flow velocity (MV) and pulsatile amplitude (PA) were determined from the resulting flow velocity contour. Responses of pulmonary microvessels to hypercapnia were examined by measuring the vessel diameters with an ocular microscale of the microscope while gas mixtures were applied to a 1-mm-diameter region of the surface. During hypercapnia both MV (2.31 +/- 0.27 mm/s) and PA (0.54 +/- 0.15 mm/s) in the alveolar arterioles (luminal diameter = 64 +/- 14 microns) were reduced, each reaching a minimum (2.01 +/- 0.24 and 0.43 +/- 0.19 mm/s, respectively) prior to gradual returns to their initial values. After reintroduction of the control gas, the values of MV and PA approached initial values more rapidly. In capillaries MV (1.44 +/- 0.18 mm/s) and PA (0.28 +/- 0.06 mm/s) decreased to 1.25 +/- 0.10 and 0.15 +/- 0.05 mm/s, respectively. The maximum reduction of PA (-44.6%) therefore clearly exceeded that of MV (-12.4%) in capillary flow. An analog model calculation suggested that the reduction in diameter of the arteriolar system could reduce PA more than MV in the pulmonary capillary network. The time course of the velocity change closely resembled that of the diameter change in relatively large arterioles. Vasoconstriction of the arterioles therefore appeared to be the major cause of these decrements in MV and PA.

A Model for an Acoustically Driven Microbubble Inside a Rigid Tube

2014 ◽  
Vol 137 (2) ◽  
Author(s):  
Adnan Qamar ◽  
Ravi Samtaney
Keyword(s):  
Bubble Radius ◽  
Coupled Model ◽  
Tube Diameter ◽  
Navier Stokes ◽  
Navier Stokes Equation ◽  
Rigid Tube ◽  
Basic Model ◽  
Proposed Model ◽  
D 12 ◽  
Bubble Fragmentation

A theoretical framework to model the dynamics of acoustically driven microbubble inside a rigid tube is presented. The proposed model is not a variant of the conventional Rayleigh–Plesset category of models. It is derived from the reduced Navier–Stokes equation and is coupled with the evolving flow field solution inside the tube by a similarity transformation approach. The results are computed, and compared with experiments available in literature, for the initial bubble radius of Ro = 1.5 μm and 2 μm for the tube diameter of D = 12 μm and 200 μm with the acoustic parameters as utilized in the experiments. Results compare quite well with the existing experimental data. When compared to our earlier basic model, better agreement on a larger tube diameter is obtained with the proposed coupled model. The model also predicts, accurately, bubble fragmentation in terms of acoustic and geometric parameters.

Simulation and Intelligent Control of Stratified Flow Control Sink

2014 ◽  
Vol 644-650 ◽  
pp. 171-174
Author(s):  
Lei Rao ◽  
Wei Wei Tao
Keyword(s):  
Flow Control ◽  
Flow Velocity ◽  
Intelligent Control ◽  
Effective Range ◽  
Flow State ◽  
Simulation Data ◽  
Interactive Interface ◽  
Control Of Flow ◽  
Set Up ◽  
Flow States

This article proposes a sink which is multi-circulating stratified control of flow velocity. We research the different effective range of one certain flow state with changing velocity of each layer of the sink and obtain several typical flow states with changing velocity combination There are some changes of effective range between different velocities through studying the different flow states. We can get expected flow states in different combinations. Then we use neutral network and the simulation data to realize the intelligent control and set up a friendly interactive interface.

Numerical Simulation Calculation of Hydroplane Direct Route Motion Based on FLUENT

2012 ◽  
Vol 569 ◽  
pp. 368-375
Author(s):  
Yu Qin ◽  
Xiao Liang ◽  
Jia Ning Zhang
Keyword(s):  
Numerical Simulation ◽  
Performance Prediction ◽  
Dynamic Pressure ◽  
Hydrodynamic Performance ◽  
Navier Stokes ◽  
Navier Stokes Equation ◽  
Velocity Change ◽  
Direct Route ◽  
Field Situation ◽  
Simulation Calculation

Aiming at hydrodynamic performance prediction for hydroplane motion, numerical simulation calculation for direct route motion of a hydroplane was carried out under FLUENT software platform by using VOF method and RNG k-ε model and solving Navier-Stokes equation. Evolution of ship resistance was obtained as the velocity change, and flow field situation and dynamic pressure variation of hydroplane hull bottom were reflected intuitively. By comparing the results of FLUENT calculation and ship model experiment and theoretical estimation, analyzing, especially wake current, it was verified that numerical simulation calculation of hydroplane direct route motion and hydrodynamic performance prediction based on FLUENT are feasible and precise enough.

scholarly journals The Impact of Air–Sea Interactions on the Predictability of the Tropical Intraseasonal Oscillation

2008 ◽  
Vol 21 (22) ◽  
pp. 5870-5886 ◽  
Author(s):  
Kathy Pegion ◽  
Ben P. Kirtman
Keyword(s):  
Zonal Wind ◽  
Climate Model ◽  
Intraseasonal Oscillation ◽  
Coupled Model ◽  
Longwave Radiation ◽  
Boreal Winter ◽  
Potential Predictability ◽  
Key Factor ◽  
The Impact ◽  
Tropical Intraseasonal Oscillation

Abstract This study investigates whether air–sea interactions contribute to differences in the predictability of the boreal winter tropical intraseasonal oscillation (TISO) using the NCEP operational climate model. A series of coupled and uncoupled, “perfect” model predictability experiments are performed for 10 strong model intraseasonal events. The uncoupled experiments are forced by prescribed SST containing different types of variability. These experiments are specifically designed to be directly comparable to actual forecasts. Predictability estimates are calculated using three metrics, including one that does not require the use of time filtering. The estimates are compared between these experiments to determine the impact of coupled air–sea interactions on the predictability of the tropical intraseasonal oscillation and the sensitivity of the potential predictability estimates to the different SST forcings. Results from all three metrics are surprisingly similar. They indicate that predictability estimates are longest for precipitation and outgoing longwave radiation (OLR) when the ensemble mean from the coupled model is used. Most importantly, the experiments that contain intraseasonally varying SST consistently predict the control events better than those that do not for precipitation, OLR, 200-hPa zonal wind, and 850-hPa zonal wind after the first 10 days. The uncoupled model is able to predict the TISO with similar skill to that of the coupled model, provided that an SST forecast that includes these intraseasonal variations is used to force the model. This indicates that the intraseasonally varying SSTs are a key factor for increased predictability and presumably better prediction of the TISO.

SIMULASI ARUS LALU LINTAS DENGAN MENGGUNAKAN KECEPATAN MODEL KERNER KONHÄUSER

2016 ◽  
Vol 5 (2) ◽  
Author(s):  
Yessy Yusnita
Keyword(s):  
Finite Difference ◽  
Flow Velocity ◽  
Traffic Flow ◽  
Stokes Equation ◽  
Navier Stokes ◽  
Real Situation ◽  
Navier Stokes Equation ◽  
Conservation Equations ◽  
The Real ◽  
Road Section

In the real situation, the vehicle flow velocity on a road are not always in an equilibrium situation. The Kerner Konhäuser model illustrate that the vehicle flow velocity is an application of the Navier Stokes equation. The model is solved numerically by using the finite difference approach to calculate the flow velocity. The result will be used in solve the conservation equations in order to the density of traffic flow. The Simulation is carried on a single-lane road section. The results show that the vehicle flow velocity will increase if the density of the traffic flow decreases and the vehicle flow velocity will decrease if the density of traffic flow increases.

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