1. Introduction
Over the years, a variety of parametric wind profile models have been developed to depict representative tangential wind and/or pressure profiles within a tropical cyclone. Originally introduced to tropical meteorology by Depperman (1947), a Rankine (Rankine 1882) vortex model was used in numerous studies to approximate the inner core of solid-body rotation of the tropical cyclone (TC). Outside the core, the tangential wind decreased, with some values of about 0.6 ± 0.1 being inversely proportional to radius from the TC center. The velocity distributions were found to give a good approximation to the tangential wind profiles of TCs (Hughes 1952; Riehl 1954, 1963; Malkus and Riehl 1960, among others). Although the modified Rankine model had some observational support (Gray and Shea 1973), the model did not allow computation of a relation between the maximum wind and minimum sea level pressure because the radial integral of the gradient wind acceleration was not bounded at a large radius (Willoughby and Rahn 2004).
Schloemer (1954) proposed an alternative model in which a TC surface pressure field was assumed to follow a modified rectangular hyperbolic function with radius, and the gradient-balance wind was calculated from the radial variation of hurricane pressure. Myers (1957) adopted the Schloemer model to derive a pressure–wind relation in which the maximum balanced wind was proportional to the square root of the pressure difference between large radius and the TC center. Adopting the Schloemer model, Holland (1980) introduced an additional parameter, now commonly referred to as the Holland B parameter, into an inverse exponential function of radius to represent a parametric pressure field. The field in turn must be differentiated with respect to radius to obtain a gradient wind. This parameter was critical in allowing the pressure profile, and thus the controlling width of the wind profile spanning the maximum, to accommodate the gamut of velocity shapes typically found in mature TCs. The Holland model, however, suffers from two major shortcomings, as noted by Willoughby and Rahn (2004): (i) the areas of strong inner winds in the eyewall and of nearly calm winds at the storm center were unrealistically wide compared to observations, and (ii) the outer winds outside the eyewall decayed too rapidly with increasing radial distance from the center. Lack of extensive reconnaissance aircraft datasets prior to 1980s apparently contributed to the shortcomings of the Holland model. Since then, modern technologies produce better datasets that offer much potential for increased knowledge about detailed TC wind profiles including multiple-maxima concentric-eyewall tangential winds. As a result, the datasets led Holland et al. (2010) to improve the original Holland (1980) model by (i) allowing the wind equation exponent to vary in order to fit outer wind observations, and (ii) adding a secondary wind profile to the preexisiting primary wind profile. Their discussion on secondary wind maxima, however, was superficial because it was unclear how variability of outer wind (i.e., secondary wind) profiles was related to changes in TC intensity, strength, and/or size during an eye replacement cycle.
Two shortcomings of the Holland (1980) model led Willoughby et al. (2006, hereafter WDR) to develop a different parametric model that was designed specifically to fit wind observations and has been extensively tested on reconnaissance aircraft data. The WDR model outperformed the Holland model by increasing a number of parameters to characterize and obtain an optimum fit to complex observed wind profiles. One profile was a piecewise, continuous approximation defined by three different functions in different parts of the TC wind structure. Inside the eye, the first function used a power of radius to control the shape of the inner profile. Within the eyewall, the second function used a smooth, radially varying polynomial ramp function to replace the unrealistic discontinuity (i.e., cusp) in the infinitesimal radial thickness of the Rankine tangential velocity maximum with a smooth polynomial transition joining the inner and outer profiles. Outside the eyewall, the third function used a dual exponential to control two different decay rates of the outer profile: (i) the rapid wind decay close to the eyewall and (ii) the slow wind decay farther away from the eyewall. Using reconnaissance aircraft data, the radial profiles of tangential wind and geopotential height were shown to be able to fit well the observed profiles of flight-level tangential wind and geopotential height. Additionally, in his unpublished work with the WDR model, Willoughby successfully developed multiple-maxima wind profiles that resembled to those in Hurricane Allen (1980).
The Holland B parameter cannot model all TCs at all times because this limited parameter ranges from 0.75 to 2.5, as noted by Willoughby and Rahn (2004), WDR, Vickery and Wadhera (2008), and Vickery et al. (2009a,b) in their discussion of parametric characteristics of the Holland model. The Holland B formulation is so rigid that it is difficult to have control over the shape of the different regions of the radial distribution of the gradient wind. The difficulty of the model provides motivation to apply the Wood and White (2011) parametric tangential wind profile model (developed for high Rossby number vortices such as thunderstorm mesocyclones and tornadoes) to a TC and determine whether the model is capable of achieving an optimum fit to realistic TC pressure and multiple-maxima, concentric-eyewall tangential wind profiles with and without the eyewall replacement cycle (ERC).
The objective of this study is to extend the existing parametric tangential wind profile model of Wood and White (2011) to tailor the model for TC applications. In section 2, the following five key model parameters controlling the radial profile of tangential wind are described: maximum velocity, radius of the maximum, and three shape velocity parameters that independently control different portions of the profile. Physical interpretations of each shape velocity parameter are described. The description follows the computation of a model gradient wind from a cyclostrophic wind approximation formulated in terms of a cyclostrophic Rossby number. Section 3 discusses partitioning of the radial profile of model TC gradient and cyclostrophic winds into as many as three wind maxima. The total surface pressures are partitioned into separate components of pressures that correspond to triple wind maxima. Additionally, the partitioned central surface pressure deficits corresponding to three peak tangential wind profiles are derived. Mathematical formulas for gradient and cyclostrophic vorticity for multiple wind maxima are developed and discussed in section 4. Section 5 both uses a TC wind structural variability [similar to the Merrill (1984) concept] and a TC emulator to present a discussion on the manner in which a model TC intensifies, strengthens, and changes size by examining the behaviors of central surface pressure deficits and radial profiles of cyclostrophic and gradient winds, vorticity, and surface pressure with and without an ERC. Finally, conclusions and future work are presented in section 6.
Our parametric TC tangential wind profile model is a part of our research to obtain an optimum fit to radial profiles of aircraft flight-level data. If the parametric model successfully replicates the general aspects of observed profiles of wind and pressure (or geopotential height) in TCs, then we will eventually apply the model to azimuthal variations of high-resolution Doppler velocity signatures of vortices for various applications such as developing statistics of vortex wind profiles for use in enhancing the National Weather Service warnings.
2. Parametric modeling of TC gradient–cyclostrophic winds
a. Wood–White parametric wind model
The parametric model (1) assumes a circular wind flow pattern and does not adequately depict the actual surface boundary layer winds. Surface boundary layer winds including wind reduction factor, storm translation effects, and the degree of overwater wind axisymmetry and asymmetry (e.g., Kepert 2001, 2006a,b) could be added to the model for use in storm surge models, models of wind-driven seas, and other oceanic responses to TCs.
b. Physical interpretations
Figure 1 shows how each shape velocity parameter (
The
The
The radial profile families of normalized tangential velocity as functions of
Users/analysts interested in applying this parametric model to some actual data or simulations are encouraged to experiment with each of adjustable shape velocity parameters (
c. Gradient versus cyclostrophic wind approximations
According to Willoughby (1990b) and Willoughby and Rahn (2004), the typical local cyclostrophic Rossby numbers
When
3. Partitioned pressure–wind profiles
a. Partitioned wind profiles for multiple-maxima eyewall tangential wind profiles
Based on the seminal work of Willoughby et al. (1982), intense symmetric TCs have been observed to exhibit multiple, well-defined wind maxima during ERCs. Two (three) concentric eyewalls were defined by two (three) tangential wind peaks in each of the aircraft radial legs and by two (three) well-defined rings of enhanced radar reflectivity located at different radii from the centers of the TCs. An echo-free moat and a saddle-shaped wind profile were situated between each pair of concentric eyewalls. Good examples of the primary, secondary, and tertiary tangential wind maxima within concentric eyewalls were also provided in McNoldy (2004) and Sitkowski et al. (2011), which displayed flight-level tangential wind profiles observed by aircraft in Hurricanes Juliette (2001) and Frances (2004), respectively. According to Sitkowski et al. (2011), several TCs exhibiting multiple wind maxima show evidence of multiple ERCs. Figure 4a provides an example from Hurricane Frances (2004). The weakening primary wind maximum (identified by 1) was associated with a decaying primary (inner) concentric eyewall, while the intensifying secondary wind maximum (identified by 2) was associated with a developing secondary (first outer) concentric eyewall as an ERC neared its completion. The tertiary wind maximum (identified by 3) appeared to originate from spiral rainbands that ultimately arranged into a tertiary (second outer), well-defined concentric eyewall from which an additional ERC arose. There have been no documented cases of more than three well-defined tangential wind peaks in aircraft profiles of TCs.
b. Cyclostrophic wind balance
c. Partitioned pressure profiles for multiple-maxima eyewall tangential wind profiles
d. Partitioned central surface pressure deficits for multiple-maxima eyewall tangential wind profiles
4. Partitioned gradient and cyclostrophic vorticity for multiple-maxima eyewall tangential wind profiles
5. TC simulation results
This section uses a TC simulator to provide what each input parameter (
Merrill (1984) pioneered the use of TC wind structural variability in terms of intensity, strength, and size. Intensity is measured by minimum sea level pressure or maximum azimuthal wind in the primary vortex core; outer core wind strength is a spatially averaged tangential wind speed over an annulus between 100 and 250 km from the TC center (Weatherford and Gray 1988a,b); and size is the axisymmetric extent of gale-force (17 m s−1) wind or the average radius of the outermost closed isobar (ROCI). These are illustrated in Fig. 5 as changes from an initial tangential wind profile (dashed curve).
There is little confusion that arises concerning the term “core intensity” surrounding the RMW (Fig. 5). The term does not indicate clearly how variability in the inner wind profile and/or in the shape profile straddling the maximum is related to a change in intensity. The term could be rectified by replacing core intensity by inner core average winds. For instance, tangential wind distributions have U-, V- and bowl-shaped structures (e.g., Fig. 1a) in the inner core of intense, mature hurricanes, as seen in numerous examples of the flight-level profiles of tangential wind (Willoughby et al. 1982 among others) as well as the radial profiles of numerically evolving tangential wind, vorticity, and surface pressure minimum (Schubert et al. 1999; Kossin and Schubert 2001; Hendricks et al. 2009). Some of the distributions in the primary eyewall exhibit the broadly profiles of tangential wind (e.g., Fig. 1c); others display the peaked profiles, noted by WDR. We use surface pressure minimum as a proxy for intensity because it is our goal, via our equation (17), to investigate how a change in the shape and distribution of tangential wind directly affects intensity, strength, and size. For example, a transition of one shape profile into a different shape profile might produce a change in intensity, strength, and/or size as one goes progressively either (i) from top to bottom of Fig. 2 or from left to right, or (ii) from the initial broadly peaked profile (dashed curve) to the final sharply peaked profile (solid curve) in Fig. 5.
From extensive aircraft measurements, Willoughby (1990a,b, 1991, 2011) found that the gradient wind balance was a good approximation to the azimuthally averaged tangential winds in most portions of an inner eyewall above a boundary layer where the strong radial inflows dominate. The National Oceanic and Atmospheric Administration/Atlantic Oceanographic and Meteorological Laboratory/Hurricane Research Division (NOAA/AOML/HRD) flight-level data archive (Willoughby and Rahn 2004) provided consistent wind and geopotential height observations in hurricanes as functions of azimuth and time at fixed pressures. By averaging over azimuth and allowing for linear variation of the wind and geopotential height at fixed radii with time, these data provided an improved depiction of the time-varying azimuthally symmetric structure at a single level over 4–6 h (Willoughby 1990a,b). The maximum of the mean wind and its radius determined in this fashion were consistent estimates of RMW and
The individual wind profiles that made up the mean varied from it in interesting ways. They were generally not in gradient balance and many (if not most) of the individual profile wind maxima were stronger than the azimuthal mean maximum, but at different radii. The mean-wind profile was generally broader than the profiles that composed it because these maxima fell at different radii. As reported in the TC literature, many (but not all) of the supergradient winds appeared as the results of asymmetric radial decelerations (Kepert 2001; Kepert and Wang 2001) when analyzed in this way. A key strength of this analysis was that the variations among the observed profiles can be treated as perturbations (nonnecessarily linear) on a well behaved, nearly balanced mean vortex.
Since translation of the TC and the degree of overwater wind asymmetry were not accounted for in the model, the model TC was assumed to be axisymmetric and stationary in a quiescent, tropical environment (i.e., no external atmospheric influences or ocean interaction). The cyclone was assumed to be positioned at 20°N latitude in this study. This latitude was close to the average latitude of 23.7°N based on their climatological analyses of Knaff and Zehr (2007). Note that this mean latitude is only representative of the Atlantic basin.
Table 1 lists the selected parameter values used for our 12 experiments. The main reason for presenting the side-by-side panels in Figs. 6–11 is to compare the impact of changing one (or more) input parameter (e.g.,
Model parameter values that produced the radial profiles of
a. Hurricanes with single-maximum eyewall tangential winds
A tropical storm illustrates a nondeveloping TC when the shape velocity parameters of
A change in
It is vital to point out that (3) is optimized to describe a relatively peaked eyewall wind maximum. Because of the way the cyclostrophic Rossby number
Figures 7–9 provide what the model parameters (
1) Variable
Idealized tangential wind profiles are constructed with constant
2) Variable
A change in
3) Variable
Numerical TC simulations revealed variability in the shape of inner profiles of tangential wind, vorticity, and surface pressure near the TC center (Schubert et al. 1999; Kossin and Schubert 2001; Hendricks et al. 2009). To mimic such a shape profile, we explore the role in shaping the inner wind profile by making
In hurricane D, the tangential wind distribution inside the RMW (Fig. 8a) exhibits the bowl-shaped profile; the corresponding vorticity profile (Fig. 8b) may be described as a thin annulus of strongly enhanced vorticity embedded in the primary eyewall with relatively weak vorticity in the eye and outside the eyewall. This profile results from barotropic instability near the RMW (Schubert et al. 1999). The simulated profiles of tangential wind (Fig. 8a) and vorticity (Fig. 8b) resemble the radial distributions of numerically evolving tangential wind and vorticity (Kossin and Schubert 2001, their Figs. 3 and 11; Hendricks et al. 2009, their Fig. 3) and the flight-level profiles of tangential wind and vorticity observed in Hurricanes Guillermo (1997) and Gilbert (2008) of Kossin and Schubert (2001, their Fig. 1).
Corresponding to the vorticity profile (Fig. 8b), the
A transition from a U-shaped to a V-shaped profile of tangential wind inside the primary eyewall over a period of a few hours or less was documented by Kossin and Eastin (2001) who used aircraft flight-level data to investigate the kinematic and thermodynamic distributions within the eye and eyewall of Hurricane Diana (1984). The changes in the inner wind profile result in measurable and physically important differences in the eyewall vorticity (Fig. 8b) and central surface pressure (Fig. 8c).
Croxford and Barnes (2002, their Fig. 13a) observed the U-shaped profiles of storm-relative tangential wind in the primary eyewall of Hurricane Emily (1993), although the profiles remained nearly unchanged and the primary tangential wind maxima increased intensity from 0700 through 1000 to 1600 UTC. During this 9-h period, the RMW slowly contracted inward the TC center. Unfortunately, the radial profiles of corresponding surface pressure in this hurricane were not documented, even though Croxford and Barnes (2002) showed that increased tangential wind maximum decreased the central surface pressure minimum, as is consistent with Figs. 7a,c.
In view of the above, the variable
4) Variable
In the last experiment, the radial profiles were compared by varying
5) Variable
Now that we comprehend how the different
Figure 9 illustrates the role of
Conversely, when
Based on the simulation results in hurricanes F (G), an increase (a decrease)
Table 2 is summarized to illustrate the details of the experimental hurricanes B–G including model parameters in terms of the tangential wind profile, corresponding total surface pressure minimum, intensity, and size changes.
Details of the tangential wind profile experiments including vortex parameters and results in terms of the TC wind profile, corresponding central (total) surface pressure minimum, and intensity changes. The arrow
b. Major hurricanes with dual-maximum eyewall tangential winds
A new outer eyewall in response to convective heat release induces a new secondary tangential wind
In hurricane H, the developing secondary wind increases the strength (Fig. 10a) and intensity by decreasing the surface pressure minimum (Fig. 10c), even when the primary wind remains unchanged. It is notable that the
The TC continues to grow and strengthen during the transition from hurricane H to hurricane I, as dual inspection between Figs. 10a,d shows. As the strength continues to increase and the secondary eyewall slowly contracts inward (not shown), the radial profiles of
Another important feature in Figs. 10c,f is that the product of
The evolution of the wind profiles from hurricane I to hurricane J is illustrated in the top panels of Figs. 10d and 11a, respectively. When the inner eyewall collapses, the TC decreases intensity as the strength in the secondary eyewall continues to increase. The TC then increases intensity again as the former secondary eyewall transitions into the primary eyewall that continues to intensify. According to Willoughby et al. (1982), the total surface pressure (
There is a subtle similarity between the simulated profiles of tangential wind and pressure in Figs. 10a,c,d,f and radial profiles of the flight-level tangential wind and 700-hPa geopotential height observed by aircraft in Hurricane Allen (1980) [Figs. 4 and 15 of Willoughby et al. (1982)]. There is also a resemblance between the simulated profiles and the flight-level (450-m altitude) tangential wind and surface pressure profiles from aircraft observations of Hurricane Hugo (1989) in Figs. 11a and 15 of Marks et al. (2008). The simulated profiles of primary and secondary tangential wind and vorticity (Figs. 10d, e) resemble the flight-level profiles from aircraft observations of Hurricane Gilbert (1988) of Kossin et al. (2000, their Fig. 1b).
In summary, Fig. 12 presents evolution of a simple ERC. The radial profiles of
c. Major hurricanes with triple-maximum eyewall tangential winds
Triple concentric eyewalls consisting of three complete rings of enhanced radar reflectivity with echo-free moats have been rarely documented. Typhoon June (1975) may be the first reported case of triple eyewalls observed by reconnaissance aircraft (Holliday 1976). McNoldy (2004) documented the radial profiles of the triple concentric eyewalls observed by aircraft in Hurricane Juliette (2001). Sitkowski et al. (2011) documented that Hurricane Frances (2004) (see Fig. 4) and Hurricane Ivan (2004) exhibited triple-maximum tangential winds during the ERCs.
To simulate a simple TC with triple-maximum tangential winds, a new radial profile of a tertiary tangential wind
Concurrent with changes in the radial tangential wind distributions in major hurricane K, the
The subtly depressed pressure (kink) at
The marked kinks reflected in the simulated surface pressure profiles (Fig. 11f) resemble those observed in Hurricane Frances (2004) (Fig. 4b), particularly at 35 km on the left side of the eye and 40 km on the right side. Based on our simulations, the slightness of the tertiary kinks in Frances’ pressure profile (located at 95 km on the left side and 115 km on the right side) may be explained by the weak but developing tertiary wind and vorticity maxima associated with the developing tertiary ring of radar reflectivity.
More research is needed on the climatological characteristics of tertiary wind profiles including the wind maxima in association with tertiary eyewalls. The question needed to be addressed is as follows: Do the tertiary eyewall structures associated with tertiary tangential wind maxima have the same characteristic circulation and structures as the primary and secondary concentric eyewalls? This is important because anticipating changes in TC intensity due to multiple ERCs is one of the most challenging aspects of TC forecasting.
6. Conclusions and future work
The new parametric TC wind profile model has been developed by tailoring the Wood and White (2011) parametric tangential wind profile for TC applications. The model avoids the problem of the unbounded radial integral of the Coriolis term in gradient wind balance as the outer limit of integration to calculate the pressure profile approaches infinity. A gradient wind
The TC simulations demonstrate that the parametric model is capable of reproducing the representative results of flight-level winds and pressures as measured or inferred by aircraft reconnaissance data. The main conclusions of this study are as follows:
The
variable, as expected, is shown to be sensitive to intensity and size by increasing the magnitude, while other variables (i.e., , , , and ) remain unchanged. The
variable, while other variables are constant, is shown to be relatively insensitive to intensity and size of the inner and outer wind profiles. The
variable, termed as the growth parameter, is shown to be sensitive to intensity by controlling the linearity and nonlinearity of the inner tangential wind profile inside the RMW only, while other variables are fixed. When , a V-shaped (linear) profile is produced and related to the inner core of solid-body rotation. When increases from 1.0, the V-shaped profile transitions to bowl- to U-shaped (nonlinear) profiles, the central width of wind calm is increased at the TC center, and the surface pressure minimum rises. Additionally, vorticity concentration is displaced from the center to some radius where the strongest gradient of the inner profile occurs. The resultant vorticity profile exhibits a ring of strongly enhanced vorticity embedded in the primary eyewall with relatively weak vorticity in the eye and outside the eyewall. This profile satisfies the necessary condition of barotropic instability within the eyewall (Schubert et al. 1999). The
variable, termed as the decay parameter, is shown to be sensitive to intensity by controlling the size of the outer wind profile outside the RMW only, when other variables are held constant. Since is inversely proportional to the outer wind profile, a decrease in increases intensity by decreasing the central surface pressure deficit and increasing the size of the outer circulation at large radius. Provided that the radial profiles of the partitioned outer wind components are known, the decay parameter may be a useful parameter in measuring the ROCI and radii of 34-, 50-, and 64-kt wind (Demuth et al. 2006). The
variable, termed as the size parameter, is shown to be sensitive to intensity by controlling the radial width of the entire (inner and outer) wind profile encompassing the maximum, while other variables remain constant. An increase in transitions from a sharply to broadly peaked wind profile, thereby increasing TC intensity and the size of both inner and outer profiles concurrent with the central surface pressure fall.
A single wind profile employing five key parameters can be partitioned into as many as triple wind maxima. The definitions of
For any realistic axially symmetric TC wind profile with a single maximum, it is possible to adjust the parameters (
Our near-future work will include application of the parametric model to radial profiles of reconnaissance aircraft wind and pressure (or geopotential height) data. A fitting algorithm using the data to fit the wind and pressure profiles will involve minimizing a cost function. The results will enable us to evaluate the distributions of the fitted parameters and critically examine the fitted profile’s realism in comparison with observed tangential wind and pressure/geopotential height profiles in varying stages of TCs.
Potential applications of the TC parametric model include analytical or numerical model initialization for wind specification, hurricane risk model (e.g., Vickery and Twisdale 1995), model of wind-driven sea and other oceanic response to TC (e.g., Phadke et al. 2003), storm-surge inundation (e.g., Jelesnianski 1966), climatology of intensity and wind structure and pressure changes associated with ERCs (e.g., Sitkowski et al. 2011), and others. Also, it is possible for the parametric model to construct a two-dimensional horizontal wind and pressure fields for such applications.
Acknowledgments
The lead author would like to thank Neal Dorst of NOAA/AOML/HRD for his assistance in accessing the flight-level aircraft data of Hurricane Frances (2004). Particular thanks are extended to Corey Potvin of NOAA/OAR/NSSL for providing editorial assistance in the earlier version of the paper. The authors appreciate the constructive comments and suggestions provided by Pat Harr of the Naval Postgraduate School, John Knaff of NOAA/NESDIS Regional and Mesoscale Meteorology Branch, and another anonymous reviewer.
APPENDIX
Determination of the Decay Parameter η in a Mature TC
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Using the binomial series for the square root term and ignoring higher-order terms, it can be shown that