Numerical Prediction of Thermal Effect on Flow Field around a High-Rise Building Model

2014 ◽  
Vol 554 ◽  
pp. 680-685
Author(s):  
Fatemeh Behrouzi ◽  
Adi Maimun Abdul Malik ◽  
Nor Azwadi Che Sidik ◽  
Mehdi Nakisa ◽  
Afiq Muhammad Yazid Witri
Keyword(s):  
Thermal Effect ◽  
Flow Pattern ◽  
Surface Boundary ◽  
Heating Wall ◽  
Surface Boundary Layer ◽  
Building Model ◽  
High Rise ◽  
Building Models ◽  
Building Wall ◽  
Strong Upward Motion

Recently, CFD (Computational Fluid Dynamics) is being more and more used in the investigation of the flow and thermal around high-rise buildings. In this study, prediction of thermal effect on flow pattern around high-rise buildings model located in the surface boundary layer was carried out using k-e turbulence model. Investigation of thermal effect on flow pattern behind the building and comparison between isothermal and non-isothermal building using standard k-e showed that the surface temperature of building wall led to a strong upward motion close to heating wall and decreased the reattachment length behind it. The model sittings of validation study was accomplished by comparing the simulation of wind flow around building models with the experimental data of Architectural Institute of Japan (AIJ) that results showed in weak wind region, standard k-e has good agreement with experimental.

Three-dimensional dynamic analyses of two Colombian high-rise buildings

1969 ◽  
Vol 59 (4) ◽  
pp. 1495-1515
Author(s):  
Gary C. Hart
Keyword(s):  
Ground Motion ◽  
Three Dimensional ◽  
Office Building ◽  
Mode Shapes ◽  
Concrete Frame ◽  
Building Model ◽  
High Rise ◽  
Building Models ◽  
Dynamic Analyses ◽  
Seismograph Station

Abstract The actual earthquake damage in two high-rise buildings in Bogota, Colombia, is compared with predicted response of four three-dimensional analytic building models. Three building models of the 24-story steel frame Bank of Bogota and one of the 29-story concrete frame Bavaria Office Building are considered. Periods and mode shapes are calculated for each building model. Maximum interstory displacements, absolute roof accelerations, story shears, and torques are calculated in each building model for three well-recorded earthquakes, one being a July 1967 earthquake in Colombia, as recorded at a nearby Bogota seismograph station. In all earthquakes, both components of ground motion were applied simultaneously.

Prediction of Wind Flow around High-Rise Buildings Using RANS Models

2014 ◽  
Vol 554 ◽  
pp. 724-729 ◽  
Author(s):  
Fatemeh Behrouzi ◽  
Nor Azwadi Che Sidik ◽  
Adi Maimun Abdul Malik ◽  
Mehdi Nakisa
Keyword(s):  
Fluid Dynamics ◽  
Experimental Data ◽  
Boundary Layer ◽  
Turbulence Models ◽  
Wind Flow ◽  
Surface Boundary ◽  
Reattachment Length ◽  
Surface Boundary Layer ◽  
High Rise ◽  
Rans Models

Recently, CFD (Computational Fluid Dynamics) is being increasingly used to investigation of the flow around high-rise buildings. In this study, prediction of wind flow around two cases high-rise buildings model placed within the surface boundary layer were carried out using various turbulence models. The accuracy of two-equation turbulence models were compared with experimental data of Architectural Institute of Japan (AIJ).as a result, all two-equation models are shown overestimation the reattachment length behind the buildings.

An Introduction to the Flow about Plane Swept-back Wings at Transonic Speeds

1960 ◽  
Vol 64 (596) ◽  
pp. 449-464 ◽  
Author(s):  
E. W. E. Rogers ◽  
I. M. Hall
Keyword(s):  
Boundary Layer ◽  
Mach Number ◽  
Flow Pattern ◽  
Surface Boundary ◽  
Pitching Moment ◽  
Surface Boundary Layer ◽  
Leading Edges ◽  
The Way

SummaryA brief survey is made of the way the flow develops about wings with leading edges swept at about 50° as the stream Mach number rises from a subsonic to a supersonic value. The shock pattern which occurs may be complex. Three aspects of the wing flow are discussed in more detail, including the possible conditions for shock-induced separation of the surface boundary layer. The effect of the changing flow pattern on the overall wing lift, drag and pitching moment is commented upon.

Prediction of Atmospheric Turbulence Characteristics for Surface Boundary Layer using Empirical Spectral Methods

2020 ◽  
Author(s):  
Yagya Dutta Dwivedi ◽  
Vasishta Bhargava Nukala ◽  
Satya Prasad Maddula ◽  
Kiran Nair
Keyword(s):  
Boundary Layer ◽  
Time Series ◽  
Surface Roughness ◽  
Wind Speed ◽  
Atmospheric Turbulence ◽  
Surface Boundary ◽  
Low Frequencies ◽  
Surface Boundary Layer ◽  
Power Spectral ◽  
Mean Wind Speed

Abstract Atmospheric turbulence is an unsteady phenomenon found in nature and plays significance role in predicting natural events and life prediction of structures. In this work, turbulence in surface boundary layer has been studied through empirical methods. Computer simulation of Von Karman, Kaimal methods were evaluated for different surface roughness and for low (1%), medium (10%) and high (50%) turbulence intensities. Instantaneous values of one minute time series for longitudinal turbulent wind at mean wind speed of 12 m/s using both spectra showed strong correlation in validation trends. Influence of integral length scales on turbulence kinetic energy production at different heights is illustrated. Time series for mean wind speed of 12 m/s with surface roughness value of 0.05 m have shown that variance for longitudinal, lateral and vertical velocity components were different and found to be anisotropic. Wind speed power spectral density from Davenport and Simiu profiles have also been calculated at surface roughness of 0.05 m and compared with k−1 and k−3 slopes for Kolmogorov k−5/3 law in inertial sub-range and k−7 in viscous dissipation range. At high frequencies, logarithmic slope of Kolmogorov −5/3rd law agreed well with Davenport, Harris, Simiu and Solari spectra than at low frequencies.

scholarly journals Aerodynamics of smooth and rough square-section prisms at incidence in very high Reynolds-number cross-flows

2021 ◽  
Vol 62 (3) ◽  
Author(s):  
Nils Paul van Hinsberg
Keyword(s):  
Reynolds Number ◽  
Cross Sections ◽  
Reynolds Numbers ◽  
Circular Cylinders ◽  
Surface Boundary ◽  
Experimental Proof ◽  
Surface Boundary Layer ◽  
Pitch Moment ◽  
The Mean ◽  
High Reynolds

Abstract The aerodynamics of smooth and slightly rough prisms with square cross-sections and sharp edges is investigated through wind tunnel experiments. Mean and fluctuating forces, the mean pitch moment, Strouhal numbers, the mean surface pressures and the mean wake profiles in the mid-span cross-section of the prism are recorded simultaneously for Reynolds numbers between 1$$\times$$ × 10$$^{5}$$ 5 $$\le$$ ≤ Re$$_{D}$$ D $$\le$$ ≤ 1$$\times$$ × 10$$^{7}$$ 7 . For the smooth prism with $$k_s$$ k s /D = 4$$\times$$ × 10$$^{-5}$$ - 5 , tests were performed at three angles of incidence, i.e. $$\alpha$$ α = 0$$^{\circ }$$ ∘ , −22.5$$^{\circ }$$ ∘ and −45$$^{\circ }$$ ∘ , whereas only both “symmetric” angles were studied for its slightly rough counterpart with $$k_s$$ k s /D = 1$$\times$$ × 10$$^{-3}$$ - 3 . First-time experimental proof is given that, within the accuracy of the data, no significant variation with Reynolds number occurs for all mean and fluctuating aerodynamic coefficients of smooth square prisms up to Reynolds numbers as high as $$\mathcal {O}$$ O (10$$^{7}$$ 7 ). This Reynolds-number independent behaviour applies to the Strouhal number and the wake profile as well. In contrast to what is known from square prisms with rounded edges and circular cylinders, an increase in surface roughness height by a factor 25 on the current sharp-edged square prism does not lead to any notable effects on the surface boundary layer and thus on the prism’s aerodynamics. For both prisms, distinct changes in the aerostatics between the various angles of incidence are seen to take place though. Graphic abstract

scholarly journals A global perspective on Langmuir turbulence in the ocean surface boundary layer

2012 ◽  
Vol 39 (18) ◽  
Author(s):  
Stephen E. Belcher ◽  
Alan L. M. Grant ◽  
Kirsty E. Hanley ◽  
Baylor Fox-Kemper ◽  
Luke Van Roekel ◽  
...  
Keyword(s):  
Boundary Layer ◽  
Ocean Surface ◽  
Global Perspective ◽  
Surface Boundary ◽  
Langmuir Turbulence ◽  
Surface Boundary Layer
Sign in / Sign up

Export Citation Format

Share Document