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Numerical Investigations of the DrivAer Car Model using Opensource CFD Solver OpenFOAM

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Abstract and Figures

A lot of the investigations in automotive aerodynamics are still based on strongly simplified generic bodies such as the Ahmed Body or the SAE body. To close the gap between these strongly simplified models and highly complex production cars the new generic DrivAer body model is introduced by the Institute of Aerodynamics and Fluid Mechanics, Technische Universitat Munchen (TUM). This current study is focused on three different DrivAer body models namely Fastback, Estateback, and Notchback and two different underbody types for each model, smooth and detailed. Hence, total 6 different models are simulated using open source CFD solver OpenFOAM at two different ground conditions, with ground and without ground effect (WGS and WoGS). All the models used in simulations are 2.5 scaled down models as compared with the actual car dimensions. The vehicle velocity considered for this numerical study is 40 m/s, Reynolds number is 4.87M and turbulence model used is k-w-SST. The mesh is generated using SnappyHexMesh (SHM) tool of OpenFOAM and it is around 11 million volume cells for the smooth underbody and 14 million volume cells for the detailed underbody. The coefficients of drag (C d) values are within 0.5% to 12% error band as compared against the experimental values published by the TUM. The coefficients of pressure (Cp) plots are comparable with experimental results and also the contribution of individual body part in overall C d values is obtained in this study. All the simulations are carried out using OpenFOAM 2.1.1 on Tata Consultancy Services (TCS) High Performance Computing facility. Keywords : DrivAer body, External Aerodynamics, OpenFOAM, SnappyHexMesh, CFD, HPC, TCS.
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1
Numerical Investigations of the DrivAer Car Model using
Opensource CFD Solver OpenFOAM
Gopal Shinde1, shinde.gopal@tcs.com, Aniruddha Joshi, joshi.aniruddha@tcs.com and Kishor Nikam,
kishor.nikam@tcs.com
Abstract:
A lot of the investigations in automotive aerodynamics are still based on strongly
simplified generic bodies such as the Ahmed Body or the SAE body. To close the
gap between these strongly simplified models and highly complex production cars
the new generic DrivAer body model is introduced by the Institute of Aerodynamics
and Fluid Mechanics, Technische Universitat Munchen (TUM). This current study is
focused on three different DrivAer body models namely Fastback, Estateback, and
Notchback and two different underbody types for each model, smooth and detailed.
Hence, total 6 different models are simulated using open source CFD solver
OpenFOAM at two different ground conditions, with ground and without ground effect
(WGS and WoGS). All the models used in simulations are 2.5 scaled down models
as compared with the actual car dimensions. The vehicle velocity considered for this
numerical study is 40 m/s, Reynolds number is 4.87M and turbulence model used is
k-w-SST. The mesh is generated using SnappyHexMesh (SHM) tool of OpenFOAM
and it is around 11 million volume cells for the smooth underbody and 14 million
volume cells for the detailed underbody. The coefficients of drag (Cd) values are
within 0.5% to 12% error band as compared against the experimental values
published by the TUM. The coefficients of pressure (Cp) plots are comparable with
experimental results and also the contribution of individual body part in overall Cd
values is obtained in this study. All the simulations are carried out using OpenFOAM
2.1.1 on Tata Consultancy Services (TCS) High Performance Computing facility.
Keywords : DrivAer body, External Aerodynamics, OpenFOAM, SnappyHexMesh,
CFD, HPC, TCS.
1Author for correspondence, Gopal Shinde, shinde.gopal@tcs.com, Tata
Consultancy Services, Pune, India
2
Introduction
Nowadays with the help of Computational Fluid Dynamics (CFD) and High
Performance Computing (HPC) Technology, vehicle aerodynamics engineers are
reducing the wind tunnel experiments and accelerating the vehicle design cycle. A lot
of the investigations in automotive aerodynamics are still based on strongly
simplified generic bodies such as the Ahmed Body. In an experimental work, Ahmed
et al. [1] set a bluff body, called the Ahmed Model, in the Gottingen open section
wind tunnel and analysed the time averaged flow behaviour for different slant angle
variations. Gilli´eron et al. [2] performed computational simulation and compared
against the experimental ones for the reference Ahmed model. Lienhart et al. [3]
performed experiments for two slant angles, 250 and 350, with slightly lower velocity
40 m/s but of the same order, with Re = 2.8E06. Later, Kapadia et al. [4],
Hinterberger et al. [5], Sinisa Krajnovic and Lars Davidson [6] and Ehab Fares [7]
also contributed to understand the Ahmed body flow physics better. Recently, Ronak
Pandya et al. [8] and Angelina Heft et al. [9] also contributed numerical observations
on Ahmed body.
These simple car models like Ahmed Body or SAE body make it easy to relate the
observed phenomena to specific areas and thus help to understand basic flow
structures. At the same time, more complex flow phenomena, e.g. at the underbody,
wheels/wheelhouses and around the rear view mirrors etc., cannot be reproduced
due to the over simplification of these geometries. On the other hand, it is usually not
feasible to investigate these phenomena on a specific production vehicle, as, due to
its short life span and restricted access, typically little validation data is available.
Recognizing the need for a model combining the strengths of both approaches,
various more or less generic models, such as the VW reference car and the MIRA
reference car, have been proposed [10]. However, while these reference cars mark a
step in the right direction, these models are still too generic to completely understand
the complex phenomena occurring at realistic vehicles.
To close this gap, the Institute of Aerodynamics and Fluid Mechanics of the
Technische Universitat Munchen (TUM), in cooperation with two major car
companies, the Audi AG and the BMW Group, has proposed a new realistic generic
car model called “DrivAer Model” [11]. The body is based on two typical medium
class vehicles (Audi A4 and BMW3 series) and includes three interchangeable tops
and two different underbody geometries to allow for a high universality. To
encourage the use of the DrivAer model in independent research projects, TUM
research group is open to share the geometry and a comprehensive experimental
database is published in different papers [12, 13].
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The aim of the current work is to use different DrivAer body models and their
experimental results to validate the opensource CFD solver OpenFOAM.
Problem Description
This current study is focused on three different DrivAer body models namely
Fastback, Estateback, and Notchback and two different underbody types for each
model, smooth and detailed as shown in Figure 1. Hence, total 6 different models
are simulated using open source CFD solver OpenFOAM at two different ground
conditions, with ground and without ground effect (WGS and WoGS). In case of
WGS, car wheels are rotating anticlockwise and road is moving in the direction of air
and in case of WoGS both car wheels and road are stationary. All the models used
in simulations are 2.5 scaled down models as compared with the actual car
dimensions. Figure 2 show a sketch and main dimensions of the fastback
configuration of the 1:2.5 DrivAer model. Different parts of the Fastback model
considered for the simulation study are as shown in Figure 3. The individual drag
contribution of these components is also calculated along with the total car drag.
The vehicle velocity considered for this numerical study is 40 m/s, Reynolds number
is 4.87E106 and turbulence model used is k-w-SST.
Fastback
Estateback
Notchback
Detailed underbody
Smooth underbody
Figure 1: DrivAer body models and different underbody types
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Computational Domain and Mesh Generation
To capture the flow around the car model the computational domain is created
around the car which often called as numerical wind tunnel as shown in Figure 4.
This computational domain is like physical wind tunnel test section. The length of the
computational domain is 28 m, width is 10 m and height is 7 m. While the length of
Figure 2: Typical dimensions of the Fastback model
Figure 3: Different parts of the Fastback model
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physical wind tunnel test section is 4.8 m, width is 2.4 m and height is 1.8 m. The
blockage ratio used in computational domain is 0.57% while in physical wind tunnel it
was 6.17%.
To capture flow physics around the car more accurately the mesh size kept near the
car is fine and becomes coarse when go away from the car as shown in Figure 5. To
achieve this variable mesh size distribution various refinement boxes are created
with different dimensions as shown in Figure 4. To capture the boundary layer
around the car, multiple layers of very fine and fine element sizes are kept around
full car and along the road which is shown in Figure 6. The y+ obtained is 30 which is
supposed to be good for incompressible simulations using OpenFoam.
SnappyHexMesh (SHM) tool was used in parallel mode for the grid generation. The
meshing was carried out on 4 cores of 32 GB workstation. The mesh generated on
smooth underbody models is about 11 million volume cells and 14 million volume
cells for the detailed underbody.
Figure 4: Different boxes of refinement around the Fastback model
Figure 5: Z-Cut plane of the grid around the Fastback model
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Boundary Conditions and Solver Settings
Boundary conditions are implemented on the computational domain, car body, car
wheels and road. Velocity was specified at the inlet and pressure was specified at
outlet. Road was given translation speed 40 m/s in the direction of flow in simulations
with ground effect and considered stationary for without ground simulations. Car
wheels are rotating at 320 rad/s anticlockwise in simulations with ground effect and
considered stationery for without ground simulations. All other car parts are defined
as stationary walls.
“simpleFoam” solver from OpenFoam has been used for simulations.
“potentialFoam” solver is used to set pressure field in the domain. Post-processing
has been carried out using the in-built utilities sampleDict, streamlines, and
cuttingPlane. The models considered here are with wheels and mirrors and were
simulated for 10,000 iterations each. The convergence achieved was 5 decades fall
for flow variables P and U and 6 decades fall for turbulence quantities omega and k.
Convergence of drag force is also monitored and achieved upto 15 counts in last 100
iterations.
Some of the solver’s important settings are given below.
Time stepping = Steady state
Gradient scheme = Second order
Divergence scheme = Upwind (First order)
Laplacian scheme = Linear (Second order)
Interpolation scheme = Linear (Second order)
Turbulence model = K-omega-SST[15]
Pressure solver = GAMG
Figure 6: Zoomed view of the grid cut plane around the Fastback model
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Velocity solver = GaussSiedel
Non-orthogonal correctors = 2
Result Analysis
The total drag values obtained for the three models with smooth underbody
considering with and without ground effect are given in the Table 1. Table 2 shows
the drag values obtained for the three models with detailed underbody considering
with and without ground effect. Percentage error found out in the simulated drag
values is in the range of 0.5% to 12% as compared to the experimental drag values.
Simulated drag value is taken as the average of drag values of last 100 iterations.
The component wise drag plot for all configurations is as shown in Figures 7 and 8.
This plot shows the drag produced by each component, which gives us the important
insight where we should look for design changes in order to reduce the drag.
Reduction of drag directly contributes towards increase of fuel efficiency. These
component wise drag values are not readily available from experiments; however, it
is easily possible in simulations. Cp plots for the top surface of the models at y=0 are
plotted against the experimental Cp distribution as shown in Figure 9 and 10. We
have observed deviation in the simulated Cp distribution at the center of the model.
In experimental setup, at center of the model a vertical strut is mounted.
Model Type
Ground Effect
Expt. Cd
CFD Cd
% Error
Fastback
WoGS
0.254
0.2597
-2.24
WGS
0.243
0.2599
-6.95
Estateback
WoGS
0.296
0.2684
9.32
WGS
0.292
0.2840
2.73
Notchback
WoGS
0.258
0.2567
0.5
WGS
0.246
0.2565
-4.26
Model Type
Ground Effect
Expt. Cd
CFD Cd
% Error
Fastback
WoGS
0.284
0.2925
-2.99
WGS
0.275
0.3029
-10.14
Estateback
WoGS
0.318
0.3199
-0.6
WGS
0.319
0.3546
-11.16
Notchback
WoGS
0.286
0.3042
-6.36
WGS
0.277
0.3097
-11.8
Table 1: Total drag values for Smooth Underbody models
Table 2: Total drag values for Detailed Underbody models
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Figure 7: Component wise drag contribution plot for Smooth Underbody models
WoGS
WGS
WoGS
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WGS
Figure 8: Component wise drag contribution plot for Detailed Underbody models
Figure 9: Coefficient of pressure (Cp) plot for Fastback model, WoGS
Figure 10: Coefficient of pressure (Cp) plot for Fastback model, WGS
10
Conclusion
This current study is focused on 3 different models of DrivAer body namely
FastBack, EstateBack, and NotchBack and 2 different underbodies, smooth and
detailed underbody. Hence, total 6 different configurations are simulated using open
source software OpenFOAM at two different conditions with ground and without
ground effect. The coefficients of drag (Cd) values are within 0.5% to 12% error band
as compared against the experimental values published by the TUM. The
coefficients of pressure (Cp) plots are comparable with experimental results and also
the contribution of individual body part in overall Cd values is obtained in this study.
There are huge flow separation / recirculation zones on the back-side of the models.
In order to capture the flow features more accurately, we need to refine the grid in
these zones. Since the flow features in these zones keep on changing with respect
to time, current steady state simulations may not mimic the exact flow situation.
Unsteady state flow simulations with region-wise refined grid and with more stringent
convergence criterions may give more insights.
Future Work
In this current work, steady state simulations using k-w-SST turbulence model are
carried out. We would like to investigate this further for few more turbulence models
and also with transient calculations. Grid refinement may be necessary at the back
side of the models to capture the flow separation / recirculation zones more
accurately, which needs to be investigated.
References
1. S. R. Ahmed, G. Ramm, and G. Faltin, 1984. Some salient features of the
time averaged ground vehicle wake. SAE paper no. 840300.
2. P. Gilli´eron and F. Chometon, 1999. Modelling of stationary three-
dimensional
separated air flows around an Ahmed reference model. In ESAIMproc.,
volume 7, pages 173-182.
3. H. Lienhart, C. Stoots, and S. Becker, 2000. Flow and turbulence structures in
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the wake of a simplified car model (Ahmed Model). In DGLR Fach Symp. der
AGSTAB.
4. S. Kapadia, S. Roy, and K. Wurtzler, 2003. Detached eddy simulation over a
reference Ahmed car model. AIAA paper no. 2003-0857
5. M. Hinterberger, M. Garcia-Villalba, and W. Rodi, 2004. Large Eddy
Simulation of flow around the Ahmed body. Lecture notes in Applied and
Computational Mechanics, The Aerodynamics of heavy vehicles: Trucks,
Buses, and Trains, R. McCallen, F. Browand, J. Ross (Springer, New York,
2004).
6. S. Krajnovic and L. Davidson, 2005. Flow Around a Simplified Car, Part 1:
Large Eddy Simulation. J. Fluids Eng. 2005, Volume 127, Issue 5.
7. Ehab Fares, 2006. Unsteady flow simulation of the Ahmed reference body
using a lattice Boltzmann approach. Computers & Fluids, Volume 35, Issues
8-9, 2006.
8. Pandya, R., Pavitran, S., Nikam, K., Singh, A., A Turbulence based
Computational Study on the Drag Breakdown of Ahmed Body, IUTAM
Symposium on Bluff Body Flows, December 12-16, 2011, IIT Kanpur, India.
Pg. 337-340.
9. A. I. Heft, T. Indingery, and N. A. Adams, Investigation of Unsteady Flow
Structures in the Wake of a Realistic Generic Car Model, 29th AIAA Applied
Aerodynamics Conference, 27 - 30 June 2011, Honolulu, Hawaii
10. Le Good, G. M., and Garry, K. P., On the Use of Reference Models in
Automotive Aerodynamics, SAE Technical Paper 2004-01-1308, 2004, doi:
10.4271/2004-01-1308.
11. Angelina I. Heft, Thomas Indinger and Nikolaus A. Adams, Introduction of a
New Realistic Generic Car Model for Aerodynamic Investigations, SAE
International, 2012-01-0168
12. Mack, S., Indinger, T., Adams, N. A., and Unterlechner, P., “The Ground-
Simulation Upgrade of the TUM Wind Tunnel,” SAE Technical Paper 2012-01-
0299, 2012, doi:10.4271/2012-01-0299.
13. J. Wojciak, P. Theissen, K. Heuler, T. Indinger, N. Adams, R. Demuth:
Experimental Investigation of Unsteady Vehicle Aerodynamics under Time
Dependent Flow Conditions - Part 2, SAE 2011 World Congress, April 12-14,
2011, Detroit, Michigan, USA, Paper 2011-01-0164
14. OpenFoam User Guide, http://www.openfoam.org/docs/user/
15. Sebastian MÖLLER, Daniele SUZZI, Walter MEILE, Investigation of the flow
around the Ahmed body using RANS and URANS with various turbulence
models, 3rd OpenFoam Workshop, Politecnico Di Milano, Milan, Italy, 10-11
July 2008.
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Acknowledgements
The authors are thankful to Angelina I. Heft et al. (Institute of Aerodynamics and
Fluid Mechanics, Technische Universitat Munchen, Germany) for sharing the DrivAer
body CAD files and for valuable suggestions during this course of work. Authors
would like to thank the TCS-HPC team for their continuous support to carry out this
exercise. Authors also acknowledge the encouragement and support extended by
Mr. Rajaravisankar Shanmugam and EIS leadership team in pursuing this initiative.
... • Interpolation scheme (interpolationSchemes): Linear (Second order). • Convective scheme (divScheme): "linearUpwind" (second order) for momentum (div(phi, U) = linearUpwind) and upwind (first order) for both k and omega (Shinde et al. 2013;Shaharuddin et al. 2017). • Turbulence model: K -omega -SST. ...
... As a result, the Cds of the baseline model in the CFD simulation and the wind tunnel experiment are 0.285 and 0.292, respectively. In addition, other comparative results of Cds with respect to the estate-back model between the CFD simulation with the K -omega -SST turbulence model and the wind tunnel experiment were provided in the previous investigations (Shinde et al. 2013;Ashton and Revell 2015. Apparently, an error of 2.4% in our CFD simulation is acceptable for the industrial automotive flows. ...
... Apparently, an error of 2.4% in our CFD simulation is acceptable for the industrial automotive flows. The errors of 2.7% and 7.1% in previous studies (Shinde et al. 2013;Ashton and Revell 2015) verify the rationality of the simulation. Moreover, it should be noted that the RANS models are typically used to evaluate the direction and magnitude of a trend with an affordable computational burden. ...
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... Thus, the study is reflected to the realistic production car. The design is based on Audi A4 and BMW 3 series (Shinde et al., 2013). Figure 3 shows the DrivAer fastback geometry chosen for the current study. ...
... Similar treatment has been used by Guilmineau (2014), where the floor under the model is made moving with the freestream velocity. A higher mean D C is obtained when the floor under the model is made as no-slip condition (Shinde et al., 2013;Ashton et al., 2016), i.e., the boundary layer is allowed to developed upstream of the model, where up to 7.0% difference in mean D C is observed. ...
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... Thus, the study is reflected to the realistic production car. The design is based on Audi A4 and BMW 3 series (Shinde et al., 2013). Figure 3 shows the DrivAer fastback geometry chosen for the current study. ...
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The aim of the “Models for Vehicle Aerodynamics” (MOVA) Project is to develop, refine, and validate the latest generation of turbulence models for selected examples encountered in vehicle aerodynamics. The validation of turbulence models requires the availability of detailed experimental data. These quantitative data should cover the most critical flow regions around a bluff car-shaped body and they should give physical quantities that can directly be correlated to the results of numerical simulations. Such experimental data were measured in the LSTM low speed wind tunnel using a 2-component laser-Doppler anemometer (LDA) mounted on a traversing system and a simplified model of a car (Ahmed model). Measurements were made for two rear vehicle body slant angles (25° and 35°) at a bulk air velocity of 40 m/s. This paper serves as a synopsis of the major results of this experimental investigation.
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The large wind tunnel at the Technische Universität München was upgraded by integrating a modular single-belt system, which enables the simulation of moving ground conditions for ground vehicle testing. Central part of this system is its large belt that moves at a maximum speed of 50 m/s. This belt not only simulates the relative motion between the model vehicle under investigation and the floor, but also drives the model's wheels. Due to its size, the wind tunnel facility is suited for testing 40 % scaled models of typical passenger cars, which are held in place by a newly designed model support system consisting of five struts: One strut to support the body of the model and four struts to hold the model's wheels on top of the moving belt. Another crucial step in upgrading the wind tunnel was to install a boundary layer scoop system to reduce the thickness of the boundary layer approaching the moving belt. All new systems were designed such that they can be moved into and out of the test section of the wind tunnel to be able to restore the old setting of the test section floor. This report addresses the key challenges we had to face during the process of upgrading the wind tunnel facility and introduces its special features and its most important sub-systems. The current report also contains results of tests we conducted to measure the distribution of the static pressure along the test section and the size of the boundary layer at different locations on top of the moving belt. Even though we did not obtain perfect conditions regarding the size of the boundary layer thickness on top of the moving belt, we still were successful in improving the scope of the wind tunnel facility in terms of ground vehicle testing.
Article
State of the art aerodynamic research of vehicles often employs strongly simplified car models, such as the Ahmed and the SAE body, to gain general insights. As these models exhibit a high degree of abstraction, the obtained results can only partly be used for the aerodynamic optimization of production vehicles. Aerodynamic research performed on specific vehicles is on the other hand often limited due to their short life span and restricted access. A new realistic generic car model for aerodynamic research-the DrivAer body-is therefore proposed to close this gap. This paper focuses on the development of the model and the first experimental results, namely force and pressure measurements of the different configurations. The experiments were performed in the recently updated Wind Tunnel A of the Institute of Aerodynamics and Fluid Mechanics at the Technische Universität München.
Conference Paper
Unsteady aerodynamic flow phenomena are investigated in a wind tunnel by oscillating a realistic 50% scale model around the vertical axis. Thus the model is exposed to time-dependent flow conditions at realistic Reynolds and Strouhal numbers. Using this setup unsteady aerodynamic loads are observed to differ significantly from quasi steady loads. In particular, the unsteady yaw moment exceeds the quasi steady approximation significantly. On the other hand, side force and roll moment are over predicted by quasi steady approximation but exhibit a significant time delay. Part 2 of this study proves that a delayed and enhanced response of the surface pressures at the rear side of the vehicle is responsible for the differences between unsteady and quasi steady loads. The pressure changes at the vehicle front, however, are shown to have similar amplitudes and almost no phase shift compared to quasi steady flow conditions. The difference between unsteady and quasi steady yaw moment proves to be independent of oscillation amplitudes between 2deg and 4deg. It is assumed that the intensity of the unsteady flow phenomena is determined by the interaction of the time scale of the model rotation and the time scale of the delayed wake flow, described by the Strouhal number. The largest magnification factors for the yaw moment are found at 140kph and 2Hz for the notchback geometry, which results in a Strouhal number of Sr=0.12. It is finally shown that the yaw moment overshoot is less pronounced for a fastback and especially for a fullback geometry, which is explained by smaller unsteady pressure variations at the rear side of the fullback.
Conference Paper
The unsteady flow structures at the rear end of a car and in its wake strongly influence its handling characteristics. State of the art research on this topic often employs strongly simplified car models, such as the Ahmed body. Due to their high degree of ab- straction, however, the insights gained cannot be fully transferred to the development of production cars. To close this gap a new reference car model for aerodynamic research - the DrivAer body - is proposed in this paper. Its geometry and validation data will be published to encourage independent studies. The investigations of both the Ahmed body and the DrivAer model are conducted both numerically and experimentally. The transient numerical simulations were carried out using Large Eddy Simulation (LES) and the Scale-Adaptive Simulation Shear-Stress Transport (SAS SST) turbulence model of the open source software OpenFOAM®. These results are compared to time-accurate surface pressure measurements and force measurements. Initial results show good agreement with existing experimental data.
Article
Large eddy simulations (LES) were made of flows around a generic ground vehicle with sharp edges at the rear end (an Ahmed body with a 25 degrees angle of the rear slanted surface). Separation of the flow at the rear results in large regions with recirculating flow. As the separation is determined by the geometry, the Reynolds number effects are minimized. Resolution requirements of this recirculating flow are smaller than those in LES of wall attached flows. These two consequences of the geometry of the body are used to predict the experimental flow at relatively high Reynolds number Recommendations are presented for the preparation and realization of LES for vehicle flows. Comparison of the LES results with the experimental data shows good agreement.
Book
For a basic ground vehicle type of bluff body, the time averaged wake structure is analysed. At a model length based reynolds number of 4.29 million, detailed pressure measurements, wake survey and force measurements were done in a wind tunnel. Some flow visualisation results were also obtained. Geometric parameter varied was base slant angle. A drag breakdown revealed that almost 85% of body drag is pressure drag. Most of this drag is generated at the rear end. Wake flow exhibits a triple deck system of horseshoe vortices. Strength, existence and merging of these vortices depend upon the base slant angle. Characteristic features of the wake flow for the low drag and high drag configurations is described. Relevance of these phenomena to real ground vehicle flow is addressed.