Modelling Effect of Rain on Aerodynamic Performance of the Ahmed Body

2022 ◽  
Author(s):  
Parth Y. Patel ◽  
Jia H. Liu ◽  
Vladimir V. Vantsevich ◽  
Roy P. Koomullil
Fluids ◽  
2020 ◽  
Vol 5 (4) ◽  
pp. 244
Author(s):  
Saber Karimi ◽  
Arash Zargar ◽  
Mahmoud Mani ◽  
Arman Hemmati

The feasibility of a single dielectric barrier discharge (SDBD) actuator in controlling flow over an Ahmed body, representing a simplified car model, has been numerically and experimentally investigated at Reynolds numbers of 7.68×105 and 2.25×105. The Ahmed body had slant angles of 25∘ and 35∘. The results showed that SDBD actuators could significantly enhance the aerodynamic performance of the Ahmed body. Several arrangements of the actuators on the slant surface and the rear face of the model were examined to identify the most effective arrangement for drag reduction. This arrangement resulted in an approximately 6.1% drag reduction. This improvement in aerodynamic performance is attributed to the alteration of three-dimensional wake structures due to the presence of SDBD, which coincides with surface pressure variations on the slant and rear faces of the Ahmed body.


2021 ◽  
Vol 13 (12) ◽  
pp. 168781402110668
Author(s):  
Haichao Zhou ◽  
Qingyun Chen ◽  
Runzhi Qin ◽  
Lingxin Zhang ◽  
Huiyun Li

As vehicle speed increases, the aerodynamic drag reduction becomes increasingly significant. The aim of this paper is to find out the effects of the wheelhouse shapes on the aerodynamics of an Ahmed body with a 35 slant angle. In this paper, based on the detached-eddy simulation method, the effects of the three classic different wheelhouse on the aerodynamic performance and near wake of the Ahmed body are presented. The mesh resolution and methodology are validated against the published test results. The results show that the front wheelhouse has a significant impact on the aerodynamic performance of the Ahmed body, leading to different aerodynamic drag forces and flow fields. Enlarging the wheelhouse cavity volume could result in a gradual increase in aerodynamic drag coefficients, the ratio of the wheelhouse cavity volume increased by 2.9% and 9.8%, the drag coefficients increased by 2.5% and 4.5% respectively. The increase in aerodynamic drag was primarily caused by flow separation in the large cavity volume wheelhouse.


Author(s):  
Kisun Song ◽  
Kyung Hak Choo ◽  
Jung-Hyun Kim ◽  
Dimitri N. Mavris

The importance of the aerodynamic performance, specifically meaning reducing both drag coefficient (CD) and lift coefficient (CL), is a growing issue in the modern automotive industry. The former is to improve fuel efficiency whereas the latter is to improve driving stability. These characteristics are quite associated with the geometric details of the external car body such that many studies are putting a lot of efforts to understand the contribution of geometrical details to the aerodynamic performance. For the design point of view, the comparison among local shape factors and the following trade-off study are essential during the early stage of the exterior design. In this paper, the qualitative and quantitative contribution of local shapes to overall aerodynamic performance is explored with a simplified vehicle model, especially the Ahmed body, by performing a multi-objective design optimization in a high-speed cruising condition. To achieve the goal of this research, Computational Fluid Dynamics (CFD) analysis is incorporated with various state-of-the-art design methodologies such as Design of Experiments (DOE), surrogate modeling, sensitivity analysis, Pareto-Optimum decision making, etc. Six design variables around the rear shapes of the Ahmed body are parameterized and populated into design space via a hybrid DOE method combining Central Composite Design (CCD) and Latin Hypercube. For CD and CL, corresponding Artificial Neural Networks (ANN) are created for the surrogate model. Then, the individual and collaborative contributions of design variables are scrutinized. For further detailed analysis, a Monte Carlo Simulation (MCS) is performed so that the empirical joint probability distribution is calculated to explore the feasible and optimum design space. Based on the simulation and analysis results, Pareto frontier is identified and multi-objective optimization is conducted to seek the best appropriate vehicle shapes for different design goals between CD and CL, which weigh on fuel efficiency and driving stability, respectively.


Author(s):  
H. Viswanathan

AbstractWe evaluate the aerodynamic performance of several passive vortex generators (VGs) placed on a standard Ahmed body, with a slant angle (α = 35º), subjected to different yawing angles (β) using RANS-based models. Rigorous validation of the numerical results is performed with previously published experimental data for (β ≤ 8º) for the Ahmed body. Our model results depict a good overall agreement with several experimental data sets. An array of different vortex generators such as the delta-winglet (DVGs), the cylindrical (CVGs) and trapezoidal (TVGs) types are introduced on to the validated model. The introduction of CVGs and DVGs tends to have a beneficial aerodynamic performance for (β = 0º). In contrast, the TVGs tend to impair the performance by producing massive flow separation over the slant for (β = 0º). Conversely, for (β > 0º), a swift transition happens with TVGs wherein the high-energy streamwise vortices that are produced tend to improve the pressure footprint, thereby reducing the overall drag. A deterioration in the performance of DVGs is predicted during (β > 4º), wherein the ‘c’-pillar vortex on the leeward side interferes with the streamwise vortical structure, which adversely influences the flow over the roof-slant edge. Overall, a maximum of ~ 8.5% and ~ 7.7% drag reduction appears to be possible with the designed CVGs and TVGs at smaller vehicle yawing conditions.


2020 ◽  
Vol 14 (4) ◽  
pp. 7369-7378
Author(s):  
Ky-Quang Pham ◽  
Xuan-Truong Le ◽  
Cong-Truong Dinh

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations using the k-e turbulence model with a scalable wall function. The numerical results for the typical performance parameters without stator splitter blades were validated in comparison with experimental data. The numerical results of a parametric study using four geometric parameters (chord length, coverage angle, height and position) of the stator splitter blades showed that the operational stability of the single-stage axial compressor enhances remarkably using the stator splitter blades. The splitters were effective in suppressing flow separation in the stator domain of the compressor at near-stall condition which affects considerably the aerodynamic performance of the compressor.


2016 ◽  
Vol 10 (4) ◽  
pp. 231
Author(s):  
Abdekarim Tebbal ◽  
Fethi Saidi ◽  
Boualem Noureddine ◽  
Bachir Imine ◽  
Benameur Hamoudi

2016 ◽  
Vol 64 (1) ◽  
pp. 65-70
Author(s):  
Naohiro IBOSHI ◽  
Noriaki ITOGA ◽  
Yasuhide YAMANAKA ◽  
Abdul KADIR, ◽  
Yuzaburou HAYASHI ◽  
...  

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi

AbstractAhmed Body is a standard and simplified shape of a road vehicle that's rear part has an important role in flow structure and it's drag force. In this paper flow control around the Ahmed body with the rear slant angle of 25° studied by using the plasma actuator system situated in middle of the rear slant surface. Experiments conducted in a wind tunnel in two free stream velocities of U = 10m/s and U = 20m/s using steady and unsteady excitations. Pressure distribution and total drag force were measured and smoke flow visualization carried out in this study. The results showed that at U = 10m/s using plasma actuator suppress the separated flow over the rear slant slightly and be effective on pressure distribution. Also, total drag force reduces in steady and unsteady excitations for 3.65% and 2.44%, respectively. At U = 20m/s, using plasma actuator had no serious effect on the pressure distribution and total drag force.


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