Iterative spectral integration algorithm: Difference between revisions
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Another upper limit is <math>k_u = 150\ \mathrm{cpm}</math> that is imposed by the spatial resolution of a commonly used shear probe. | Another upper limit is <math>k_u = 150\ \mathrm{cpm}</math> that is imposed by the spatial resolution of a commonly used shear probe. | ||
You may use a different value if your shear probe has a spatial resolution different from that reported by <ref name="macounlueck2004">{{Cite journal | |||
|authors= P. Macoun and R. Lueck | |||
|journal_or_publisher= J. Atmos. Oceanic Technol. | |||
|paper_or_booktitle= Modelling the spatial response of the airfoil shear probe using different sized probes | |||
|year= 2004 | |||
|doi= 10.1175/1520-0426(2004)021 | |||
}}</ref> | |||
At the wavenumber of <math>150\ \mathrm{cpm}</math> the spectrum of the commonly used shear probe is boosted by a factor of 10. At higher wavenumbers the spectral correction is more than a actor of 10 and it is not recommended to use wavenumbers that require even more boosting. | |||
The cut-off frequency, <math>f_A</math>, of the anti-aliasing filter used by the shear-probe sampler sets another upper limit of spectral integration, namely <math>k_u \leq f_A/U</math>. | The cut-off frequency, <math>f_A</math>, of the anti-aliasing filter used by the shear-probe sampler sets another upper limit of spectral integration, namely <math>k_u \leq f_A/U</math>. | ||
The user may impose an upper limit to exclude wavenumbers that have contaminations that are not correctable. | The user may impose an upper limit to exclude wavenumbers that have contaminations that are not correctable. |
Revision as of 20:21, 1 December 2021
Spectral integration is an iterative procedure because the bandwidth required to estimate the variance of shear depends on the rate of dissipation, the level of electronic noise in the shear-probe signal, on the wavenumber of spurious signals that were not removed by the Goodman [1] algorithm, and on the wavenumber resolution of the shear probe. The rate of dissipation is estimated using
where
The wavenumber range that is dominated by electronic noise can usually be determined from a minimum in the spectrum.
Real shear is at wavenumbers smaller than this minimum while electronic noise is usually at higher wavenumbers.
The spectral minimum may be found by fitting a low-order polynomial to the spectrum in log-log space. The wavenumber of the spectral minimum sets one of the limits on
Another upper limit is
The cut-off frequency,
The wavenumber range of the spectrum of shear depends on the rate of dissipation.
The spectrum broadens in proportion to
However, the non-dimensional spectrum
where
These spectral approximations also provide the fraction of the shear variance that is resolved at any particular non-dimensional wavenumber. For all of these analytic approximations, 95% of the variance of shear is resolved at a non-dimensional wavenumber of approximately 0.12. There is little motivation for integrating the spectrum beyond this wavenumber. This sets another upper limit to spectral integration once the rate of dissipation is known, or at least known approximately.
The upper limit of spectral integration is nearly always higher than 10 cpm. For example, when
where
The spectrum is then integrated to the lowest of these upper limits to provide an improved estimate of the rate of dissipation. It is an improved estimate because it will nearly always span a range of wavenumbers that is considerably wider than 10 cpm, which improves its statistical reliability. This improved estimate is then used to determine the fraction of the shear variance that is resolved by the upper limit of integration. The estimate is divided by this fraction to form a new estimate of
For very high rates of dissipation, such as
In this range, the spectrum rises in proportion to
References
- ↑ L. Goodman, E. Levine and and R. Lueck. 2006. On measuring the terms of the turbulent kinetic energy budget from an AUV. J. Atmos. Oceanic Technol.. doi:10.1175/JTECH1889.1
- ↑ P. Macoun and R. Lueck. 2004. Modelling the spatial response of the airfoil shear probe using different sized probes. J. Atmos. Oceanic Technol.. doi:10.1175/1520-0426(2004)021
- ↑ F. Wolk, H. Yamazaki, L. Seuront, L. and and R. Lueck. 2002. A new free-fall profiler for measuring biophysical microstructure. J. Atmos. Oceanic Technol.. doi:10.1175/1520-0426(2002)019
- ↑ N. Oakey. 1982. Determination of the Rate of Dissipation of Turbulent Kinetic Energy from Simultaneous Temperature and Velocity Shear Microstructure Measurements. J. Phys. Oceanogr.. doi:10.1175/1520-0485(1982)012
- ↑ R. Lueck. 2022. The statistics of turbulence measurements. Part 2: Shear spectra and a new spectral model Shear spectra and a new spectral model. J. Atmos. Oceanic Technol.. doi:TBD
- ↑ S. Panchev and D. Kesich. 1969. Energy spectrum of isotropic turbulence at large wavenumbers. Comptes rendus de lacademie Bulgare des sciences. doi:unknown
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