Visual demonstration of three-scale sea surface roughness under light wind conditions

During the Southern Ocean Waves Experiment (SOWEX) an aircraft carried a down-looking video camera to help document the sea surface. Reflected images of the aircraft were intermittently observed in the video recorded at 15-30-m height under light and variable wind conditions. A numerical simulation...

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Bibliographic Details
Published in:IEEE Transactions on Geoscience and Remote Sensing
Other Authors: Banner, M. (author), Churnside, J. (author), Shaw, J. (author), Vandemark, D. (author), Wright, C. (author), Jensen, Jorgen (author), Lee, Sunhee (author)
Format: Article in Journal/Newspaper
Language:English
Published: Institute of Electrical and Electronics Engineers 2005
Subjects:
Online Access:http://nldr.library.ucar.edu/repository/collections/OSGC-000-000-011-009
https://doi.org/10.1109/TGRS.2005.851633
Description
Summary:During the Southern Ocean Waves Experiment (SOWEX) an aircraft carried a down-looking video camera to help document the sea surface. Reflected images of the aircraft were intermittently observed in the video recorded at 15-30-m height under light and variable wind conditions. A numerical simulation was developed to relate image contrast to the gravity-capillary wave contribution to sea-surface mean square slope (mss). "Carnival fun-house" mirror-type distortions of the image in the absence of the gravity-capillary waves relate to intermediate-scale wave persistence when wind forcing stops. Video image estimates of mss correlated better with 36-GHz scanning radar altimeter estimates than with the wind speed measured at 30-m height. When the gravity-capillary waves disappeared in the absence of wind forcing, about one-third of the 0.0015 residual mss was contributed by the dominant waves, and about two-thirds was contributed by the 1-10-m wavelength region. Near the shores of a lake in Alaska, reflected aircraft images were also observed, indicating that the gravity-capillary wave contribution to mss was only about 0.000 001, even though the wind speed at the 160-m aircraft height was 10 m/s.