Jet pressure-spectra estimation from single-snapshot tomographic PIV

Conference Paper (2018)
Author(s)

G González (Student TU Delft)

D Ragni (TU Delft - Wind Energy)

Francesco Avallone (TU Delft - Wind Energy)

Jan Schneiders (TU Delft - Aerodynamics)

D. Casalino (TU Delft - Wind Energy)

Andrea Ianiro (TU Delft - Aerodynamics, Carlos III University of Madrid)

Research Group
Wind Energy
Copyright
© 2018 G. González, D. Ragni, F. Avallone, J.F.G. Schneiders, D. Casalino, A. Ianiro
DOI related publication
https://doi.org/10.2514/6.2018-3293
More Info
expand_more
Publication Year
2018
Language
English
Copyright
© 2018 G. González, D. Ragni, F. Avallone, J.F.G. Schneiders, D. Casalino, A. Ianiro
Research Group
Wind Energy
ISBN (electronic)
9781624105609
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

The analysis of the unsteady flow field of an axisymmetric subsonic jet at Reynolds numbers between 5,000 and 20,000 and computation of its unsteady pressure field is carried out from single snapshots of tomographic PIV measurements (acquisition rate 0.8 Hz). This is achieved by a recently developed pressure-evaluation technique based upon the vortex-in-cell (VIC) methodology. The technique allows for a finite time-marching of the instantaneous 3D velocity fields obtained from low-repetition PIV systems. A time series of velocity fields in 3D is obtained, which is integrated into unsteady pressure by use of the Navier-Stokes momentum equation. Despite the limitations in the finite-time marching of the measured structures due to the size of the acquired tomographic volume, spectra of pressure fluctuations can be extracted in a frequency range between 800Hz and 20kHz. Fair agreement was found between the experimentally computed pressure spectra and the respective values found in literature. Further work is dedicated to exploit the full potential of the technique by attempting a sound pressure level integration of the noise sources from the unsteady fields.

Files

6.2018_3293.pdf
(pdf | 1.96 Mb)
- Embargo expired in 01-01-2019
License info not available