For some time now, aerodynamics research carried out at Cranfield University’s Shrivenham Campus has made use of both experimental and numerical methods. The combination of these two disciplines has enabled greater understanding of the flow physics being studied than would have been possible through either a purely experimental or purely numerical approach. Using examples of recent research projects, this paper will discuss the synergistic role that CFD and experiments have had in our aerodynamics research programme. Early combined CFD and experimental research was primarily driven by the need for CFD validation [1]. With computational resources limited, the experimental results in the example given were used to validate CFD models of impinging jet flows. The main objective was to give globally similar results to those measured in the experiments. More recently, improved computational resources have enabled refinements to the CFD models. Whilst CFD validation is still important, these models have provided additional insight into the physical processes involved, which were not discernable from the experimental measurements [2]. In the study cited, a CFD model was developed of the jet flow-field produced by two axisymmetric convergent castellated nozzles. Experimental measurements had indicated that the castellated nozzles entrained more mass flow into the jet than the baseline design. The CFD models verified that this was the case but crucially also provided a physical explanation of the entrainment mechanism that would have been very difficult to deduce from the available experimental data. CFD models enable researchers to investigate physical processes that are almost impossible to reproduce experimentally [3]. Here the investigation concentrated on the effect of using external wheel support struts during racecar wind tunnel testing. The struts are used to mechanically decouple the car body from the ground whilst still allowing the wheels to rotate. An experimentally validated CFD model of an isolated racecar wheel and strut was used to quantify the aerodynamic interference effects between the two. The virtual environment of the CFD model enabled the support strut to be easily removed, something that could not have been carried out experimentally! In our studies on transonic cavity flows, CFD and experiments are being used in synergy to provide design input for flow control techniques. The experimental measurements are being used to provide boundary condition inputs for the CFD models. Once validated, these models are being used used to prototype flow control mechanisms, which will suppress the undesirable acoustic phenomena. The most promising CFD-based control mechanisms will then be tested experimentally.
[1]
Sung-Eun Kim,et al.
Advances in External-Aero Simulation of Ground Vehicles Using the Steady RANS Equations
,
2000
.
[2]
A.M.O. Smith,et al.
Turbulence models and their application in hydraulics: W. Rodi, University of Karlsruhe, International Association for Hydraulic Research, Rotterdamseweg 185, 2600 MH Delft, The Netherlands
,
1981
.
[3]
S. Orszag,et al.
Renormalization group analysis of turbulence. I. Basic theory
,
1986
.
[4]
P. Bradshaw,et al.
Turbulence Models and Their Application in Hydraulics. By W. RODI. International Association for Hydraulic Research, Delft, 1980. Paperback US $15.
,
1983,
Journal of Fluid Mechanics.
[5]
D. Bray,et al.
COMPUTATION OF NORMAL IMPINGING JETS IN CROSS-FLOW AND COMPARISON WITH EXPERIMENT
,
1991
.
[6]
Kevin Knowles,et al.
An Experimental and Numerical Investigation of an Open Transonic Cavity
,
2003
.
[7]
A generalised optimisation method for double pulsed particle image velocimetry
,
1997
.
[8]
S. Wereley,et al.
A PIV Algorithm for Estimating Time-Averaged Velocity Fields
,
2000
.
[9]
J. B. Baker,et al.
On the Influence of Ground Movement and Wheel Rotation in Tests on Modern Car Shapes
,
1987
.
[10]
D. Hart,et al.
PIV error correction
,
2000
.
[11]
M. Reeder,et al.
Supersonic jet mixing enhancement by vortex generators
,
1991
.
[12]
MODELLING AND EXPERIMENTS ON UNDEREXPANDED TURBULENT JET MIXING
,
2002
.
[13]
Jeff Howell,et al.
An evaluation of CFD for modelling the flow around stationary and rotating isolated wheels
,
1998
.
[14]
R. Y. Wong,et al.
Numerical modelling of mixing in underexpanded jets from castellated nozzles
,
2002,
The Aeronautical Journal (1968).
[15]
Mark F. Reeder,et al.
Effect of tabs on the flow and noise field of an axisymmetric jet
,
1993
.
[16]
A. Saddington,et al.
NUMERICAL PREDICTIONS AND EXPERIMENTS ON SUPERSONIC JET MIXING FROM CASTELLATED NOZZLES
,
2002
.