Articles | Volume 8, issue 3
https://doi.org/10.5194/amt-8-1617-2015
© Author(s) 2015. This work is distributed under
the Creative Commons Attribution 3.0 License.
the Creative Commons Attribution 3.0 License.
https://doi.org/10.5194/amt-8-1617-2015
© Author(s) 2015. This work is distributed under
the Creative Commons Attribution 3.0 License.
the Creative Commons Attribution 3.0 License.
Research article
| 
28 Mar 2015
Research article |
| 28 Mar 2015
Performance of WVSS-II hygrometers on the FAAM research aircraft
A. K. Vance
CORRESPONDING AUTHOR
Met Office, Exeter, UK
S. J. Abel
Met Office, Exeter, UK
R. J. Cotton
Met Office, Exeter, UK
A. M. Woolley
FAAM, Cranfield, UK
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17 citations as recorded by crossref.
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- Development of aerosol activation in the double-moment Unified Model and evaluation with CLARIFY measurements H. Gordon et al. 10.5194/acp-20-10997-2020
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- Small ice particles at slightly supercooled temperatures in tropical maritime convection G. Lloyd et al. 10.5194/acp-20-3895-2020
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- Retrievals of the Far Infrared Surface Emissivity Over the Greenland Plateau Using the Tropospheric Airborne Fourier Transform Spectrometer (TAFTS) C. Bellisario et al. 10.1002/2017JD027328
- The structure of turbulence and mixed-phase cloud microphysics in a highly supercooled altocumulus cloud P. Barrett et al. 10.5194/acp-20-1921-2020
- Performance of the NCMRWF convection‐permitting model during contrasting monsoon phases of the 2016 INCOMPASS field campaign A. Jayakumar et al. 10.1002/qj.3689
- Intercomparison of airborne and surface-based measurements during the CLARIFY, ORACLES and LASIC field experiments P. Barrett et al. 10.5194/amt-15-6329-2022
1 citations as recorded by crossref.
Saved (final revised paper)
Latest update: 22 Mar 2025
Short summary
Comparisons on the FAAM BAe 146-301 aircraft show good agreement between chilled mirror hygrometers and a WVSS-II fed from a modified Rosemount inlet (wvssR) in coud-free conditions, but a WVSS-II fed from the standard flush inlet (wvssF) over-reads, except at higher humidities. Case studies in cloudy conditions show that wvssF is immune to liquid water and ice, whilst wvssR is susceptible to both. Both WVSS-II inlets respond much more rapidly than the chilled mirror devices, especially wvssF.
Comparisons on the FAAM BAe 146-301 aircraft show good agreement between chilled mirror...
