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The proposed typhoon initialization scheme is based on the IAU technique. There are three steps to achieving typhoon initialization using this scheme. First, a commonly used vortex relocation method is chosen to separate the background field into the TC vortex and the environmental flow. Then, the TC vortex is relocated to its observed location. Subsequently, the wind speed of the TC vortex is adjusted according the observed MWS near the TC center, and then the adjusted TC vortex is added back into the environmental flow to obtain the updated ICs with the revised TC position and corrected TC intensity. Finally, the increments, obtained by comparing the new field and the background field before the implementation of the vortex relocation and wind adjustment procedures, are incorporated into the model's prognostic equations using the IAU method.
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The vortex relocation method primarily follows Kurihara[12]. Schematically, the scheme used to construct a realistic initial field can be expressed as follows:
$$H^{\prime}=H_{E}+H_{V}^{\prime}=H-H_{V}+H_{V}^{\prime}, $$ (1) where H/H ' is the background / analyzed field before / after the vortex relocation process, HE is the environmental field (or large-scale circulation field), HV is the vortex component (or storm component) of the storm separated from the background field, and HV' is the vortex component with the TC position adjusted.
The most important element of the procedure is the separation of the TC vortex against its environmental flow from the background fields, which can be divided into the following steps.
(ⅰ) Identify the initial TC position and covering radius of TC vortex in the background. The geopotential height field at 850 hPa is used to determine the location of TC center. Then, the angular mean wind (AMW) is calculated. As the radial distance increases, the AMW will increase monotonously to a maximum value (where the radial distance is called rmax) and then decrease monotonously. The covering radius r0 is defined as the radial distance at which the AMW is equal to a predetermined value (set at 3 m s-1 here) at the first time when the radial distance increases after rmax.
(ⅱ) Separate the perturbation field from the background field using a twice-smoothing filter technique. A three-point smoothing algorithm is performed first longitudinally and then zonally on the background field with the same smoothing coefficient as used by Yuan et al.[15] to obtain the perturbation field HD.
(ⅲ) Separate the TC vortex from the perturbation field by applying a column filter technique:
$$H_{V}(r, \theta)=[1-E(r)]\left[H_{D}(r, \theta)-\overline{H_{D}\left(r_{0}\right)}\right], $$ (2) where r is the radial distance from the TC center, θ is the azimuth of the TC system, r0 is the covering radius of the TC vortex, $\overline{H_{D}\left(r_{0}\right)}$ is the angular mean of HD at the point of r0, and E(r) is the column filter function, which can be expressed as follows:
$$E(r)=\frac{exp \left[-\left(r_{0}-r\right)^{2} / l^{2}\right]-exp \left[-r_{0}^{2} / l^{2}\right]}{1-exp \left[-r_{0}^{2} / l^{2}\right]}, $$ (3) where l is the shape parameter of E(r) (here, l = r0/5 in this work).
(ⅳ) Obtain the large-scale environmental field:
$$H_{E}=H-H_{V}. $$ (4) Finally, the obtained vortex component HV is moved to the corrected position where its vortex center agrees with the observed TC center, which is called the vortex component with the TC position adjusted HV'.
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The wind speed adjustment follows Xu et al.[32]. According to Equation (4), the wind field with the TC position adjusted can be expressed as follows:
$$\left\{\begin{array}{l}u^{\prime}=u_{E}+u_{V}^{\prime} \\ v^{\prime}=v_{E}+v_{V}^{\prime}\end{array}\right., $$ (5) where u' and v' are the zonal and meridional wind components of H', uE and vE are the zonal and meridional wind components of the large-scale environmental field HE, and uV' and vV' are the zonal and meridional wind components of the vortex component with the TC position adjusted HV', respectively.
The wind speed adjustment is conducted by multiplying a coefficient:
$$\left\{\begin{array}{l}u_{c}^{\prime}=u_{E}+\beta \times u_{V}^{\prime} \\ v_{c}^{\prime}=v_{E}+\beta \times v_{V}^{\prime}\end{array}\right., $$ (6) where uc' and vc' are the zonal and meridional wind components after adjustment, respectively. Obviously, the surface MWS calculated from uc' and vc' should be equal to the observed one Vobs:
$$u_{c, {r_0}}^{\prime\;\;\;\;2} + v_{c, {r_0}}^{\prime\;\;\;\;2} = {\left( {{u_E} + \beta \times u_V^\prime } \right)^2} + {\left( {{v_E} + \beta \times v_V^\prime } \right)^2} = {V_{{\rm{obs}}}}, $$ (7) where uc, r0' and vc, r0' are the zonal and meridional wind components after adjustment at the point where the surface wind is maximum, respectively. Thus, coefficient β can be solved as follows:
$$\beta=\frac{-\left(u_{E} u_{V}^{\prime}+v_{E} v_{V}^{\prime}\right)+\sqrt{\left(u_{E} u_{V}^{\prime}+v_{E} v_{V}^{\prime}\right)^{2}-\left(u_{V}^{\prime\;\;2}+v_{V}^{\prime\;\;2}\right)\left(u_{E}^{2}+v_{E}^{2}-V_{\text {obs}}^{\;\;2}\right)}}{\left(u_{V}^{\prime\;\;2}+v_{V}^{\prime\;\;2}\right)}, $$ (8) It should be noted that coefficient β is calculated at the surface. Based on practical experience, it is known that the wind speed error decreases gradually as the height increases. Therefore, coefficient β should change linearly to a value of 1 at 500 hPa, which means that the wind speed in the lower (higher) levels has undergone large (small) correction.
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The IAU technique incorporates analysis increments into a model integration in a gradual manner. The analysis increments are treated as constant additional forcing terms in the model's prognostic equations over a certain time window:
$$\frac{\partial F}{\partial t}=\cdots+\frac{F_{a}-F_{b}}{\tau}, $$ (9) where F is the prognostic variable, Fa is the analyzed field with the vortex relocated, Fb is the background field before the vortex is relocated, and τ is the relaxation time window. Bloom et al. proved that the IAU procedure has the attractive properties of a low-pass time filter that can affect the response of a model to the analysis increments[25]. By progressive incorporation of the analysis increments, the IAU method removes high-frequency noise (Lee et al.[26]).