Wind Stress Over the Ocean 2001
DOI: 10.1017/cbo9780511552076.002
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Cited by 7 publications
(12 citation statements)
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“…The z 0 complexity hinders the straightforward modeling of the MASL as a wall‐bounded shear flow (Prandtl, ): Ufalse/u*=1κlog()u*zν+C, where κ is Von Kármán's constant, C is an integration constant, z is height into the constant flux layer, ν is kinematic viscosity, and u * is the shear velocity ( τρ0.1emu*2). This rare, analytical fluid mechanics solution (Bradshaw & Huang, ) presumes the flow and surface are in statistical equilibrium (Hultmark et al, ; Jones et al, ). Over the ocean, the stress‐relevant roughness ( z 0 ∝ ν / u * ) is primarily carried by gravity capillary waves (Hwang, ; Laxague et al, ), which have short relaxation times relative to local forcing changes (Zhang et al, ).…”
Section: Introductionmentioning
confidence: 99%
“…The z 0 complexity hinders the straightforward modeling of the MASL as a wall‐bounded shear flow (Prandtl, ): Ufalse/u*=1κlog()u*zν+C, where κ is Von Kármán's constant, C is an integration constant, z is height into the constant flux layer, ν is kinematic viscosity, and u * is the shear velocity ( τρ0.1emu*2). This rare, analytical fluid mechanics solution (Bradshaw & Huang, ) presumes the flow and surface are in statistical equilibrium (Hultmark et al, ; Jones et al, ). Over the ocean, the stress‐relevant roughness ( z 0 ∝ ν / u * ) is primarily carried by gravity capillary waves (Hwang, ; Laxague et al, ), which have short relaxation times relative to local forcing changes (Zhang et al, ).…”
Section: Introductionmentioning
confidence: 99%
“…Jones and Toba (2001) and Donelan et al. (2012) assumed Re = 0.11 for the near‐surface laminar air flow.…”
Section: Methodsmentioning
confidence: 99%
“…The total wind stress consists of two components: the form stress τ f caused by pressure difference between the windward and leeward sides of the wave and the viscous (skin) stress τ v caused by the drag in the viscous sublayer (Donelan et al., 2012; Jones & Toba, 2001; Makin et al., 1995; Monin & Yaglom, 1971). As the aerodynamic sheltering is specifically a consequence of the wave form, τ v must be subtracted from the measured stress such that τf=ττv=ρauw2+vw2τv ${\tau }_{f}=\tau -{\tau }_{v}={\rho }_{a}\sqrt{{\left(-\overline{{u}^{\prime }{w}^{\prime }}\right)}^{2}+{\left(-\overline{{v}^{\prime }{w}^{\prime }}\right)}^{2}}-{\tau }_{v}$ …”
Section: Methodsmentioning
confidence: 99%
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“…The zonal and meridional surface vector wind stresses are calculated from the surface vector wind data, as τ=ρaCD|U10|bold-italicU10 (Smith, 1988; Trenberth et al., 1990) with ρa is the air density, bold-italicU10 is the wind speed at 10 m, and CD is the drag coefficient (Jones & Toba, 2001). The SLA, SST, and surface wind data contain the same grid information.…”
Section: Methodsmentioning
confidence: 99%