Article

Observations and model calculations of aerodynamic drag on sea ice in the Fram Strait

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Abstract

Wind and temperature profiles in the constant flux layer obtained by tethersonde were used to compute the total aerodynamic drag on an area of 60% pack ice in the Fram Strait (79°20′N, 1−3°W). The boundary layer appeared adiabatic to heights greater than 150 m, and there were only minor air/water temperature differences. Drag coefficients of 4.9 and 5.1 × 10 -3 referred to 10 m above ground level were found. Eddy correlation measurements in the local constant flux layers over ice floes were used to estimate the skin drag of an area of 100% ice cover. This was less than 40% of the total drag on the actual area. The corresponding drag coefficient was 1.4×10 -3 . A drag partition model is proposed for computing the total drag over an area of pack ice as a function of ice concentration, mean freeboard and length of the ice floes, and typical roughness lengths of ice and sea surfaces. The model predicts maximum form drag at 73% ice concentration for floes of the type observed in the Fram Strait. DOI: 10.1111/j.1600-0870.1988.tb00413.x

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... Zusätzlic ist in der Abbildung 5.14 die von Hanssen-Bauer und Gjessing (1988) an die Messungen von Nägel (1943, 1946 angenähert Abschattungsformel (2.40) eingezeichnet (nachfolgend Nägeli-Formel) welche in einigen Modellrechnungen den Abschattungseffekt im Lee von Eisschollenkanten beschreibt (z.B. Hanssen-Bauer und Gjessing, 1988, Birnbaum, 1998. ...
... Um d a s Konzept auf diabatische Schichtung zu erweitern, wird die Gleichung (2.39) verwendet, die von anderen Autoren zur Berechnung des Formwiderstandes von Schollenkanten genutzt wurde (z.B. Hanssen-Bauer und Gjessing, 1988, Birnbaum, 1998 Lensu et al. (1996) erfaBt werden konnten. Die MeBwerte werden übe Klassen der atmosphärische Schichtung gemittelt (&/L = 0.025) und überdecke mit -0.59 < z/L < 0.14 labile bis schwach stabile Bedingungen (Tabelle 6.1). ...
... Such bulk drag models have been developed by, e.g., Arya (1975) to estimate the drag caused by pressure ridges on Arctic pack ice. This model was extended by Hanssen-Bauer and Gjessing (1988) for varying sea-ice concentrations. A more general drag model was proposed by Raupach (1992), which was extended by Andreas (1995) for sastrugi, by Smeets et al. (1999) for rough ice, and by Shao and Yang (2008) for surfaces with higher obstacle density, such as urban areas. ...
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... Momentum flux atmosphere-ice The ice and upper ocean circulation in the Arctic Ocean is mainly wind driven (Thorndike & Colony, 1982). The large scale aerodynamic drag on sea ice depends on wind speed, atmospheric vertical stability, ice concentration and surface roughness (Zubov, 1943, Smith et al., 1970, Overland, 1985, Guest and Davidson, 1987, Hanssen-Bauer & Gjessing, 1988. Models are developed for computing the aerodynamic drag on ice under different conditions (Sverdrup, 1918;Overland et al., 1983;Overland and Davidson, 1991;Overland and Guest,'1991;Walter and Overland 1991), but so far there have been few experiments to test these models. ...
... [5] The parametrization of the MIZ surface roughness has been discussed intensively during the last three decades, starting with studies by Overland [1985] and Guest and 1 Davidson [1987]. A general finding of Andreas et al. [1984], Hanssen-Bauer and Gjessing [1988], Stössel and Claussen [1993], Mai et al. [1996], Birnbaum and Lüpkes [2002], Lüpkes and Birnbaum [2005], and Lüpkes et al. [2012] was that atmospheric momentum fluxes are influenced not only by the skin drag of the open water surface and of the more or less plane ice floe surfaces but also by the form drag caused by the edges of floes, where often small ridges form due to floe collisions. So, the effective atmospheric drag over the MIZ was parametrized by accounting for both skin drag and form drag using schemes of different complexity. ...
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The aerodynamic drag of Arctic sea ice is calculated using surface data, measured by an airborne laser altimeter and a digital camera in the marginal ice zone of Fram Strait. The influence of the surface morphology on the momentum transfer under neutral thermal stratification in the atmospheric boundary layer is derived with the aid of model concepts, based on the partitioning of the surface drag into a form drag and a skin drag. The drag partitioning concept pays attention to the probability density functions of the geometric surface parameters. We found for the marginal ice zone that the form drag, caused by floe edges, can amount to 140% of the skin drag, while the effect of pressure ridges never exceeded 40%. Due to the narrow spacing of obstacles, the skin drag is significantly reduced by shadowing effects on the leeward side of floe edges. For practical purposes, the fractional sea-ice coverage can be used to parameterize the drag coefficientCdn, related to the 10 m-wind. Cdnincreases from 1.2 · 10-3 over open water to 2.8 · 10-3 for 55% ice coverage and decreases to 1.5 · 10-3 for 100% ice coverage.
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The focus of this paper is on the representation of Antarctic coastal polynyas in global ice-ocean general circulation models (OGCMs), in particular their local, regional, and high-frequency behavior. This is verified with the aid of daily ice concentration derived from satellite passive microwave data using the NASATeam 2 (NT2) and the bootstrap (BS) algorithms. Large systematic regional and temporal discrepancies arise, some of which are related to the type of convection parameterization used in the model. An attempt is made to improve the fresh-water flux associated with melting and freezing in Antarctic coastal polynyas by ingesting (assimilating) satellite ice concentration where it comes to determining the thermodynamics of the open-water fraction of a model grid cell. Since the NT2 coastal open-water fraction (polynyas) tends to be less extensive than the simulated one in the decisive season and region, assimilating NT2 coastal ice concentration yields overall reduced net freezing rates, smaller formation rates of Antarctic Bottom Water, and a stronger southward flow of North Atlantic Deep Water across 30 S. Enhanced net freezing rates occur regionally when NT2 coastal ice concentration is assimilated, concomitant with a more realistic ice thickness distribution and accumulation of High-Salinity Shelf Water. Assimilating BS rather than NT2 coastal ice concentration, the differences to the non-assimilated simulation are generally smaller and of opposite sign. This suggests that the model reproduces coastal ice concentration in closer agreement with the BS data than with the NT2 data, while more realistic features emerge when NT2 data are assimilated.
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This paper estimates the air/sea drag coefficient for first-year ice from recent aircraft measurements and reconciles the range of observed drag coefficients (103CD = 1.2–3.7 referenced to 10 m) for all sea ice types, based on ice roughness and seasonal meteorology. For the purpose of sea ice modeling, it is necessary to define an effective drag coefficient which relates regional stress to regional wind, because sea ice is heterogeneous on scales less than 20 km. Regional stress is influenced by the distribution of surface roughness, the buoyancy flux from quasi-periodic leads, and external atmospheric conditions, principally the inversion height. 103CD is 1.3–1.5 for smooth ice but is much greater for nonflat surfaces. For wind speeds greater than 5 m/s and air temperatures below freezing, the effective 103CD is 2.5–3.0 for nearly continuous pack ice, such as first-year ice in seasonal ice zones and central Arctic basin. The range of values of 103CD is 3.0–3.7 for unstable boundary layers typical of off-ice winds in the marginal ice zone (MIZ) or even greater if the ice has been broken by a recent storm. CD values at the lower end of these ranges are associated with low inversion heights. These coefficients are confirmed by 103CD of 2.9, 2.5, and 3.1 for first-year sea ice calculated from gust probe data collected by the NOAA P-3 aircraft, interior to the inner MIZ in the Bering Sea during the Marginal Ice Zone Experiment (MIZEX-West) in February 1983, and 103CD of 2.6 for the Arctic calculated from Arctic Ice Dynamics Joint Experiment (AIDJEX) aircraft data for February 1976. The effective drag coefficient with the presence of even a small concentration of sea ice is greater than the oceanic value as shown by a 103CD of 2.2 calculated from NOAA P-3 gust probe data over a 40-km track of 0.4 ice concentration in the outer MIZ of the Greenland Sea in June 1984 during MIZEX-84. The relation of surface wind and stress to the geostrophic wind for shallow inversion heights, typical of high latitudes, is reviewed with a turbulent closure atmospheric boundary layer model. The winter Arctic is typified by low inversions (
Article
For a free-drift case a method is developed for simultaneously determining air (Ca) and water (Cw) drag coefficients by solving the vertically integrated stress balance equation for sea ice. The method allows the algebraic determination of Ca and Cw from measurements of relative wind and relative current at single reference levels, from estimates of the densities of all three fluids and ice thickness, and from estimates of the accelerations caused by the nonsurface stress terms derived from position measurements. The method treats the ice as a natural drag plate and therefore includes contributions from both skin and form drag. One shortcoming of the technique is that if the relative wind and current are colinear, then only the ratio of Ca and Cw can be determined. Another is that the accelerations caused by other forces need to be independently determined. An experiment was conducted on a single floe in the eastern Bering Sea over the continental shelf during March 1981. The site was about 80 km from the ice edge and was occupied for approximately 3 days following the passage of a storm which had broken the pack into 10-20 m diameter floes. Both profile and slab inversion estimates of drag were made from the current meter and anemometer measurements at the site: Ca at 3 m was 4.55×10-3 by the profile method, compared to 3.63-4.39×10-3 for slab, depending on assumptions; Cw at 1.1 m by profile was 24.2×10-3, compared to 18.3-22.0×10-3 for slab. The two methods gave results which were not statistically separable and which were among the highest drags observed for sea ice. The instantaneous stress balance on the floe included contributions from material acceleration, Coriolis force, the two surface stresses, and sea-surface tilt relative to mean current and tide.
Article
Wind velocity and temperature fluctuations have been recorded over a large, flat, snow covered ice floe in the Gulf of St. Lawrence using sonic anemometer-thermometers. Reynolds stresses and heat fluxes have been computed digitally by the eddy correlation method. The average drag coefficient, C10 = 0.0014, is the same as that of the sea surface and about half that of moderately rough ice. Spectra and cospectra of velocity and temperature fluctuations are expressed in dimensionless forms, and coherence cospectra of the fluctuations at various lateral separations are examined.
Article
During a traverse of the Antarctic marginal ice zone (MIZ) near the Greenwich Meridian in October 1981, we launched a series of radiosondes along a 150-km track starting at the ice edge. Since the wind was from the north, off the ocean, these radiosonde profiles showed profound modification of the atmospheric boundary layer (ABL) as the increasing surface roughness decelerated the flow. The primary manifestation of this modification was a lifting of the inversion layer with increasing distance from the ice edge by the induced vertical velocity. But there was also a cooling of the stably stratified mixed layer below the inversion and a consequent flux of sensible heat to the surface that averaged over 200 W/m2. The magnitude of this flux suggests that atmospheric heat transport plays a significant role in the destruction of ice in the Antarctic MIZ. Using the rising of the inversion and ABL similarity theory, we estimated the change in the neutral stability drag coefficient, CD, across the MIZ. CD increased from its open ocean value, 1.2×10-3, at the ice edge to 4.0×10-3 at 80-90% ice concentration. We present an equation for this dependence of drag on ice concentration that should be useful for modeling the surface stress in marginal ice zones.
Article
Turbulent flux measurements were made at four levels (42, 90, 195, and 340 m) by the NOAA P-3 aircraft over first-year sea ice in the northern Bering Sea during February 1982. Three profiles of momentum flux and mean wind were used to calculate an air-ice drag coefficient CD of 3.0 ± .6 × 10-3 referenced to a 10-m anemometer height. The boundary layer was slightly unstable (zi/L = -1.2, where zi, was the inversion height of 660 m and L the Monin-Obukhov length). The mean wind speed at the 42-m height was 17 m/s, and the air temperature was -20°C. From turbulent heat flux measurements the value of the bulk heat transfer coefficient CH was 0.73 ± 1.6 × 10-3, giving a CH/CD of 0.24. The Bowen ratio was greater than 2.8. Comparison of the present turbulent flux and variance profiles with those collected over the ocean shows agreement, which increases confidence in the calculations. The geostrophic drag coefficient |u*|/|G|, where u* is the friction velocity and G is the geostrophic wind, was 0.047. The turning angle of the surface wind (measured by an anemometer at a height of 3 m on the ice) was 32°, and the ratio of surface wind speed to the geostrophic wind speed was 0.76.
Article
A simple drag partition theory is developed for the classical problem of boundary layer flows over regular arrays of two- or three-dimensional roughness elements. The theoretical expression for the ratio of the form drag on these elements to the total drag is shown to be in good agreement with wind tunnel observations. It is used for determining the contribution of form drag on pressure ridges to the total wind stress on the arctic pack ice. The theory also leads to an expression for the large-scale roughness parameter as a function of mean ridge height, ridging intensity, small-scale or local roughness parameter, and an average form drag coefficient. It is required for determing the average wind stress over large areas of the Arctic on a routine basis, using the so-called geostrophic drag method, as envisaged in the Aidjex program.
Article
Various methods of measuring air stress on the arctic ice surface are discussed; however, none of them could possibly take into account the form drag due to pressure ridges. An expression is derived for the form drag per unit area in terms of certain key parameters of ridge statistics and a suitable drag coefficient. By using the available field and laboratory measurements of these parameters an estimate is made of the ratio of the form drag to the frictional stress. It depends on the geographical location in the Arctic, the season of the year, and the meteorological conditions in the atmospheric surface layer. It is found, contrary to the common assumption, that the form drag on pressure ridges may be much larger than the frictional stress on the ice surface, especially under stably stratified conditions.
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The influence of the roughness length on calculated fluxes of momentum and matter in the boundary layer is discussed. From observations of the velocity profiles of wind and water current, the roughness length of arctic sea ice is found to vary greatly around an average of 0.02 cm for the upper and 2 cm for the lower surface.
Article
Measurements of the momentum flux were made by the Reynolds flux and dissipation methods on a deep water stable tower operated by the Bedford Institute of Oceanography . A modified Gill propeller-vane anemometer was used to measure the velocity. Drag coefficients from 196 Reynolds flux measurements agree well with those previously reported. Based on 192 runs, a comparison of the dissipation and Reynolds flux results shows excellent agreement on average, for wind speeds from 4 to 20 m sSUB-SUB1. The much more extensive dissipation data set (1086 h from the tower and 505 h from the weathership PAPA, CCGS Quadra) was used to investigate the dependence of the drag coefficient on wind speed, fetch and stability. Some time series of the momentum flux and drag coefficient are shown to demonstrate additional sources of variation in the drag coefficient. (from authors' abstract)
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The partition of the total shearing stress, [tau], between that contribution attributable to the roughness elements projecting from a wind tunnel wall, , and the shearing stress at the intervening wall surface, [tau]g, is expressed as: , where F is the total wall area of which F' is not covered by roughness elements.
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