Estimation of unsteady aerodynamic forces using pointwise velocity data
Estimation of unsteady aerodynamic forces using pointwise velocity data
A novel method to estimate unsteady aerodynamic force coefficients from pointwise velocity measurements is presented. As opposed to other existing methodologies, time-resolved full velocity fields are not required. The methodology is based on a resolvent-based reduced-order model which requires the mean flow to obtain physical flow structures and pointwise measurement to calibrate their amplitudes. A computationally affordable time-stepping methodology to obtain resolvent modes in non-trivial flow domains is introduced and compared with previous existing matrix-free and matrix-forming strategies. The technique is applied to the unsteady flow around an inclined square cylinder at low Reynolds number. The potential of the methodology is demonstrated through good agreement between the fluctuating pressure distribution on the cylinder and the temporal evolution of the unsteady lift and drag coefficients predicted by the model and those computed by direct numerical simulation
Gomez, F.
3cd7f89a-64df-4c02-b5c5-f6823cdf3180
Sharma, A.S.
cdd9deae-6f3a-40d9-864c-76baf85d8718
Blackburn, H.M.
ae789033-1e30-4261-91a6-fd2e136b0ff3
11 October 2016
Gomez, F.
3cd7f89a-64df-4c02-b5c5-f6823cdf3180
Sharma, A.S.
cdd9deae-6f3a-40d9-864c-76baf85d8718
Blackburn, H.M.
ae789033-1e30-4261-91a6-fd2e136b0ff3
Gomez, F., Sharma, A.S. and Blackburn, H.M.
(2016)
Estimation of unsteady aerodynamic forces using pointwise velocity data.
Journal of Fluid Mechanics, 804.
(doi:10.1017/jfm.2016.546).
Abstract
A novel method to estimate unsteady aerodynamic force coefficients from pointwise velocity measurements is presented. As opposed to other existing methodologies, time-resolved full velocity fields are not required. The methodology is based on a resolvent-based reduced-order model which requires the mean flow to obtain physical flow structures and pointwise measurement to calibrate their amplitudes. A computationally affordable time-stepping methodology to obtain resolvent modes in non-trivial flow domains is introduced and compared with previous existing matrix-free and matrix-forming strategies. The technique is applied to the unsteady flow around an inclined square cylinder at low Reynolds number. The potential of the methodology is demonstrated through good agreement between the fluctuating pressure distribution on the cylinder and the temporal evolution of the unsteady lift and drag coefficients predicted by the model and those computed by direct numerical simulation
Text
1606.04739v1.pdf
- Accepted Manuscript
Text
estimation-of-unsteady-aerodynamic-forces-using-pointwise-velocity-data.pdf
- Version of Record
Restricted to Repository staff only
Request a copy
More information
Accepted/In Press date: 13 August 2016
e-pub ahead of print date: 8 September 2016
Published date: 11 October 2016
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 401422
URI: http://eprints.soton.ac.uk/id/eprint/401422
ISSN: 0022-1120
PURE UUID: faf3b39a-06d8-4466-83db-19266412dc97
Catalogue record
Date deposited: 13 Oct 2016 12:43
Last modified: 15 Mar 2024 05:58
Export record
Altmetrics
Contributors
Author:
F. Gomez
Author:
A.S. Sharma
Author:
H.M. Blackburn
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics