Bernoulli equation and flow over a mountain
- Wen-Yih Sun^{1, 2, 3}Email author and
- Oliver M. Sun^{4, 5}
https://doi.org/10.1186/s40562-015-0024-1
© Sun and Sun; licensee Springer. 2015
Received: 30 December 2014
Accepted: 10 April 2015
Published: 9 June 2015
Abstract
The Bernoulli equation is applied to an air parcel which originates at a low level at the inflow region, climbs adiabatically over a mountain with an increase in velocity, then descends on the lee side and forms a strong downslope wind. The parcel departs from hydrostatic equilibrium during its vertical motion. The air parcel can be noticeably cooler than the temperature calculated from adiabatic lapse rate, which allows part of enthalpy to be converted to kinetic energy and produces a stronger wind at mountain peak and a severe downslope wind on the lee side. It was found that the hydrostatic assumption tends to suppress the conversion from enthalpy to kinetic energy. It is also shown that the Froude number defined in the atmosphere is equal to the ratio of kinetic energy to the potential energy, same as in Boussinesq fluid. But in the atmosphere, the Froude number cannot be used to determine whether a parcel can move over a mountain or not, unless the vertical motion is weak and the system is near hydrostatic equilibrium. Numerical simulations confirm that except in highly turbulent areas, the potential temperature and Bernoulli function are almost conserved along the streamline, as well as the change of kinetic energy comes from the change of enthalpy instead of potential energy.
Keywords
Background
Severe downslope winds on the lee sides of mountains have been observed frequently around the world. They may trigger dust storms in the Taklimakan Desert and Gobi Desert (Sun et al., 2013a, b). Several hypotheses have also been proposed to explain these winds, including: (a) hydraulic jump: if the mountain height exceeds a certain threshold, a strong wind can develop along the lee when a subcritical flow transitions to a supercritical flow (Long 1953; Peltier and Clark 1979; Smith 1985; Durran 1986; Baines 1995; Doyle et al. 2000; Lin 2007). The hydraulic jump was originally derived from shallow-water equations; (b) superposition of upward- and downward-propagating waves: Klemp and Lilly (1975) suggested that strong downslope winds occur when the atmosphere has a multilayer structure that produces an optimal superposition of upward- and downward-propagating waves; (c) wave breaking and enhancement of downslope winds by the energy trapped by the wave-breaking region in the upper layer and/or wave-induced critical layer (Clark and Peltier 1977, 1984; Peltier and Clark 1979; Smith 1989; Aihara and Hirasawa 1988; Lin 2007). Because the numerical simulations with a nonslip surface could not simulate the long-lasting severe windstorms observed in Boulder from the conventional theories, Sun (2013) has proposed a new theory: (d) geostrophic adjustment of the geostrophic-unbalanced upper-level jet introducing a convergence in the upper layer and enhancing the downslope wind. Sun’s numerical simulations reproduced a long-lasting, strong downslope wind (~50 m s^{−1}) on the lee side over a nonslip surface. More detailed discussions are referred to Sun (2013).
The Bernoulli equation in a two-layer fluid is a popular explanation for the formation of hydraulic jump. The Bernoulli equation has also been used to study the development of blocking flows as well as aerodynamic and hydrodynamic problems (Clancy 1975). Long (1953, denoted as L53 hereafter) presented a mathematically linear equation governing steady mountain waves of large amplitude in an incompressible fluid (Smith 1985, denoted as S85 hereafter). S85 also used an incompressible Bernoulli equation to calculate the severe downslope wind in the lee of a mountain. Although the assumption of incompressibility and hydrostatic equilibrium is useful for obtaining analytical solutions, nonhydrostatic, nonlinear numerical models in fully compressible fluid show that dynamic pressure can be significant for realistic flows moving over a mountain; however, these effects are ignored in the models of L53, S85, and others. The numerical simulations also confirm that, over a free-slip surface, the Bernoulli equation holds well for an isentropic flow over a mountain before it reaches high-turbulence regions on the lee side. However, the simulated density is not a constant along a constant Bernoulli line.
According to the Bernoulli equation, the energy needed for a parcel to climb over a mountain can come from both kinetic energy and enthalpy. Therefore, the conventional Froude number, i.e., Fr = U/Nh where U is the basic flow speed, N the Brunt–Väisälä frequency, and h the mountain height, may not be appropriate to represent this energy conversion in a stratified, compressible fluid flow. Through Bernoulli equation, we prove that the conventional Froude number does represent the ratio between kinetic energy and potential energy in a compressible fluid.
It is noted that the Bernoulli equation is only exact for an inviscid, steady flow. It is also noted that a small area of returning flow near the surface on the windward side may propagate upwind with time. In highly turbulent regions on the lee side, the flow may become unsteady too. Our nonlinear numerical model requires eddy viscosity and weak smoothing to ensure numerical stability in simulating flow over a high mountain. However, the impacts of smoothing and viscosity are found to be insignificant except in turbulent regions or near the surface when a nonslip surface is used. Numerical results show that conservations of Bernoulli function (which is related to the total energy of an air parcel and is defined as B in Methods) and potential temperature hold quite well before the flow encounters highly turbulent regions on the lee side of the mountain. In nonslip surface cases, above the surface frictional layer, the simulated B, potential temperature, and streamlines are near-parallel, and Bernoulli function and potential temperature conservation also hold quite well.
Methods
The Bernoulli equation derived from the Navier–Stokes equations consists of the kinetic energy, potential energy, and enthalpy. The analytical solutions also reveal that when an air parcel moves over a mountain, the change of kinetic energy comes from the change of enthalpy instead of from the potential energy, which invalids the popular theory of hydraulic jump based on the conversion between potential energy and kinetic energy. The detailed deviations also show that the conventional Froude number cannot be applied to estimate the mountain height a flow can climb over because it ignores the change of enthalpy.
Numerical simulations obtained from National Taiwan University–Purdue University nonhydrostatic model show the detailed structure of the flow passing a mountain, including an increase of velocity near the mountain peak and a strong downslope wind on the lee side where the temperature and pressure are relatively lower than the surroundings. They also show that potential temperature, streamline, and Bernoulli function almost remain constant following the trajectory of an air parcel, but wind, pressure, and density changes significantly.
Results and discussion
Basic equations and analytic solutions
Because (∇ × V) × V is orthogonal to d r, (∇ × V) × V • d r = 0.
where c _{ p } dT = d h, and h (specific enthalpy) = c _{ v } T + p/ρ, where c _{ v } is the specific heat at constant volume. Hence, Bernoulli function may be considered as the total energy, i.e., the summation of the kinetic energy, enthalpy, and potential energy (PE).
where the density ρ is replaced by the initial value ρ _{ i } (z, x = 0) in Eq. (11a) following L53, and ρ _{ c } = 1 kg m^{−3} in Eq. (11b) according to S85. The simulated Bernoulli function, potential temperature, and streamlines generated from a nonlinear numerical model are almost parallel before reaching high-turbulence regions or near a nonslip surface. This implies that the flow is nearly adiabatic, inviscid, and steady in the areas we are interested. The contours of B _{L} of Eq. (11a) will be presented as well for comparison in the next section.
where β _{ad} ≡ g/c _{ p } is the dry adiabatic lapse rate, which is frequently used to calculate the change of the air parcel temperature due to compression/expansion during hydrostatic–adiabatic vertical motions.
Property of air parcel along constant B at 1A, 1B, ..,4C: and \( {T}_{i,f}^{\mathrm{ad}}(K)={T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}(K)={T}_{\mathrm{A}}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{A},\mathrm{B}} \) at row 1B, \( {T}_{i,f}^{\mathrm{ad}}(K)={T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}={T}_{\mathrm{B}}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{B},\mathrm{C}} \) at 1C, \( {T}_{i,f}^{\mathrm{ad}}(K)={T}_{\mathrm{A}*,\mathrm{B}*}^{\mathrm{ad}}={T}_{\mathrm{A}*}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{A}*,\mathrm{B}*} \) 1B*, etc., for cases 1–4 at different locations
Case + location | x (km) | z (m) | p (hPa) | θ (Κ) | T (K) | B (m^{z}s ^{−2}) | U (m s^{−1}) | \( {T}_{i,f}^{\mathrm{ad}}(K)={T}_i-{\beta}_{\mathrm{ad}}\Delta {z}_{i,f} \) | ρ (kgm^{−3}) | Kinetic energy (m^{Z} s^{−2}) | \( {C}_p\left({T}_{i,f}^{\mathrm{ad}}-T\right)\left({\mathrm{m}}^{\mathrm{z}}{\mathrm{s}}^{\hbox{-} 2}\right) \) | KE_{ f } − KE_{ i } (m^{Z} s^{−2}) |
---|---|---|---|---|---|---|---|---|---|---|---|---|
1A | 160 | 1099. | 748.659 | 291.1 | 268.01 | 280,000 | 11.24 | 0.9733 | 63.12 | |||
1B | 320 | 2391. | 628.278 | 291.1 | 254.91 | 280,000 | 31.89 | 255.40 | 0.8588 | 508.9 | 487.9 | 445.7 |
1C | 348 | 378.0 | 795.373 | 290.7 | 272.30 | 280,000 | 74.44 | 274.56 | 1.0178 | 2771. | 2272. | 2263. |
1D | 347 | 1087. | 730.587 | 325.2 | 297.29 | 309,930 | 35.90 | 0.8563 | 645.9 | |||
1A* | 160 | 253.9 | 832.548 | 286.9 | 272.24 | 276,007 | 10.39 | 1.0656 | 54.00 | |||
1B* | 320 | 2061. | 656.594 | 286.9 | 254.36 | 276,007 | 24.41 | 254.60 | 0.8994 | 298.13 | 234.9 | 244.1 |
2A | 160 | 1123. | 744.034 | 291.3 | 267.67 | 279,890 | 4.037 | 0.9685 | 8.154 | |||
2B | 320 | 2227. | 641.966 | 291.3 | 256.65 | 279,890 | 22.94 | 256.90 | 0.8715 | 262.3 | 250. | 254.2 |
2C | 340 | 562.3 | 776.768 | 291.3 | 271.01 | 279,890 | 65.61 | 272.90 | 0.9987 | 2155. | 1898. | 1892. |
2A* | 160 | 582.9 | 796.686 | 289.3 | 271.10 | 278,039 | 2.183 | 1.0239 | 2.393 | |||
2B* | 320 | 2061. | 656.197 | 289.3 | 256.52 | 278,039 | 18.22 | 256.67 | 0.8913 | 166.1 | 155.6 | 163.7 |
3A | 160 | 531.3 | 798.692 | 287.4 | 269.55 | 276,000 | 8.159 | 1.0325 | 33.28 | |||
3B | 320 | 2139 | 647.706 | 287.4 | 253.84 | 276,000 | 10.71 | 253.86 | 0.8891 | 57.45 | 17.07 | 24.16 |
3C | 353 | 305.1 | 819.443 | 287.4 | 271.52 | 276,000 | 23.23 | 271.74 | 1.0516 | 270.0 | 220.9 | 212.5 |
4A | 160 | 2870. | 588.768 | 295.7 | 254.15 | 283,597 | 18.55 | 0.8072 | 172.0 | |||
4B | 320 | 3149. | 565.735 | 295.7 | 251.31 | 283,597 | 24.16 | 251.43 | 0.7844 | 292.5 | 119.5 | 120.5 |
4C | 332 | 1087 | 737.338 | 295.6 | 270.99 | 283,597 | 38.19 | 271.42 | 0.9481 | 739.2 | 436.7 | 446.7 |
where N is the Brunt–Väisälä frequency.
where g’ = gθ’/θ is the reduced gravity and \( \overline{\theta} \) is the environmental potential temperature (Baines 1995). It is noted that variation of pressure is not included in the equation of state in Boussinesq fluid, i.e., ρ’/ρ = −θ’/θ. The reciprocal of the Froude number (Nh/U _{ i }), the nondimensional mountain height, is defined by some meteorologists as a measure of nonlinearity for the continuously stratified flow over topography, instead of Froude number because they argued that U/Nh does not represent the ratio of KE and PE as originally defined in the shallow-water fluid for the flow over bottom topography (Lin 2007). On the other hand, (21) confirms that U/Nh in a stratified fluid flow does represent the ratio of KE change and PE change, as that defined in the shallow water; thus, it is appropriate to call it Froude number.
Equation (20) implies that U _{ f } = (2KE_{ f })^{1/2} should be less than U _{ i } if the air parcel pressure is the same as the surrounding environment, which is in hydrostatic equilibrium.
which is consistent with \( {\mathrm{KE}}_f-{\mathrm{KE}}_i={c}_p\left({T}_{i,f}^{\mathrm{ad}}-{T}_f\right) \) _{.} More detail will be presented in Results and discussion.
Similarly, the air over the mountain peak descends and accelerates to fill the mass deficit on the lee side created by blocking of the mountain. The wind speed also increases as long as its temperature is cooler than that calculated from adiabatic lapse rate. This has been confirmed by the nonlinear numerical model and will be presented in Results and discussion.
where \( p\hbox{'}={p}_f-{p}_{i,f}^{\mathrm{ad}} \) and \( \rho \hbox{'}={\rho}_f-{\rho}_{i,f}^{\mathrm{ad}} \). Hence, if T ' ≠ 0, both p’ and ρ’ are also different from zero, where p’ can be interpreted as the dynamic pressure.
Model and numerical simulations
The National Taiwan University–Purdue University nonhydrostatic model simulations are used for comparison with the analytical results discussed in the previous section. The prognostic variables are potential temperature, velocity, density, turbulent kinetic energy, etc. The detailed equations, physics, parameterizations, and numerical schemes of the model can be found in Hsu and Sun (2001), Sun and Hsu (2005), and Sun (2013). Following Sun et al. (2012, 2013c), we also partially filter the high-frequency acoustic waves to permit a larger time interval while solving for internal gravity waves, since the model uses a time-splitting technique.
where p _{0}, the pressure in the reference atmosphere, is a function of height. The domain consists of 671 × 400 grids with a uniform horizontal spatial interval dx = 1 km, and a vertical spatial interval, dz ≈ 75 m, except the first layer above the ground where dz ≈ 25 m. Both free-slip and nonslip surfaces are applied at the ground. In addition to Newtonian damping applied to the upper layers, the top is set at ≈30 km, higher than in most models, to reduce spurious reflections from the top boundary, which could produce standing waves and artificially enhance the downslope wind in the numerical model. The variables are fixed at the inflow, x = 0; and an open boundary is used at the outflow. An idealized mountain with a Witch-of-Agnesi profile h = h _{ m }/{(x − x _{ o })/a]^{2}} is centered at x _{ o } = 320 km with characteristic width ɑ = 10 km, and height h _{ m } = 2 km (Doyle et al. 2000; Hsu and Sun 2001; Sun and Hsu 2005; and Sun 2013). A free-slip surface is applied to cases 1–3, and a nonslip surface is applied to case 4.
Case 1: U = 20 m s^{−1}, and β = 3.5 K km^{−1} for z < 12 km, and β = 0.7 K km^{−1} for z > 12 km at inflow.
We can follow the trajectory of an air parcel along B = 280,000 m^{2} s^{−2}, which passes 1A (x = 160 km, z = 1099.14 m) in the upstream region, where θ = 291.1 K, T = 268.01 K, U = 11.24 m s^{−1}, and ρ = 0.9733 kg m^{−3}; 1B (x = 320 km, z = 2391 m) over the mountain peak where θ = 291.1 K, T = 254.91 K, U = 31.89 m s^{−1}, and ρ = 0.8588 kg m^{−3}; and 1C (x = 348 km, z = 378 m) with strong downslope wind, U = 74.44 m s^{−1}, θ = 290.7 K, T = 272.30 K, and ρ = 1.0178 kg m^{−3}, as shown in Table 1. Fig. 1a, b also shows that, near the mountain top, the wind becomes stronger but the temperature is lower than in the surrounding air. The temperature at 1C is also cooler than its surroundings.
Rows 1A, 1B, and 1C of Table 1 confirm that potential temperature remains almost constant along a constant B-function, which implies conservation of θ and B to be a good approximation, as shown in Fig. 1a, b. The temperature at 1B, T _{1B} = 254.91 K is less than the temperature of a parcel rising from 1A to 1B following adiabatic lapse rate, \( {T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}={T}_{\mathrm{A}}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{A},\mathrm{B}}=255.40\mathrm{K} \). Hence, U = 31.89 m s^{−1} at 1B over the mountain top is much stronger than U = 11.24 m s^{−1} at 1A in the lower upstream region. The temperature at 1C, T _{C} = 272.30 K is also less than \( {T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}={T}_{\mathrm{B}}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{B},\mathrm{C}}=274.56\mathrm{K}, \) while U = 74.44 m s^{−1} at 1C is stronger than U = 31.89 m s^{−1} at 1B. Table 1 also shows the difference in KE between 1A and 1B, KE_{B} − KE_{A} = 445.7 m^{2} s^{−2}, and the difference in enthalpy \( {c}_p\left({T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}-{T}_{\mathrm{B}}\right) \) = 487.9 m^{2} s^{−2} at 1B. The difference of kinetic energy between 1B and 1C is 2263 m^{2} s^{−2} and \( {c}_p\left({T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}-{T}_{\mathrm{C}}\right) \) is 2272 m^{2} s^{−2} at 1C, in good agreement with Eq. (16). Fig. 1a and Table 1 also show that the severe downslope winds on the lee side originate from z ≈ 1.1 km instead of from mid-level (4–6 km) at x ≈ 160 km, because the increase of U depends on the change of enthalpy, \( {c}_p\left({T}_{i,f}^{\mathrm{ad}}-{T}_f\right) \), instead of gΔz.
Notably, the wind is relatively weak over the warm spot at 1D (x = 347 km, z = 1087 m) where B = 309,930 m^{2} s^{−2}, θ = 325.197 K, T = 297.29 K, and U = 36.9 m s^{−1} as shown in row 1D of Table 1 and Fig. 1b. This warm spot with a weak wind is created by adiabatic subsidence warming, associated with a large descent from the mid-atmosphere. By contrast, the velocity in an incompressible fluid would be greater with increasing drop height.
Rows of 1A* and B* in Table 1 show that the parcel with B = 276,007 m^{2} s^{−2}, θ = 286.9 K, T = 272.24 K, and U = 10.39 m s^{−1} from the inflow region at 1A* (x = 160 km, z = 253.9 m) moves to the mountain top 1B* (x = 320 km, z = 2061 m) with B = 276,007 m^{2} s^{−2}, θ = 286. 9 K, T = 254.36 K, and U = 24.41 m s^{−1}. The potential temperature θ remains almost constant along B = 276,007 m^{2} s^{−2}. The wind at 1B* is much stronger than that at 1A* while the pressure and temperature are lower than the environment as shown in Fig. 1b. The simulated temperature at 1B*, T _{1B*} = 254.36 K, is lower than. \( {T}_{\mathrm{A}*,\mathrm{B}}^{\mathrm{ad}}={T}_{\mathrm{A}*}-{\beta}_{\mathrm{ad}}\varDelta {z}_{\mathrm{A}*,\mathrm{B}*}=254.60\mathrm{K}. \) The KE difference between 1A* and 1B* is 244.1 m^{2} s^{−2} and is also very close to \( {c}_p\left({T}_{\mathrm{A}*,\mathrm{B}*}^{\mathrm{ad}}-{T}_{\mathrm{B}*}\right) \) = 250.0 m^{2} s^{−2} at 1B* according to Eq. (16).
Along B = 280,000 m^{2} s^{−2} at 1A, 1B, and 1C, θ remains around 291.1 K, but the density changes considerably following the motion (i.e., dρ/dt ≠ 0); density also changes noticeably but θ remains near 286.9 K along B = 276,007 m^{2} s^{−2} at 1A* and B*. This differs significantly from dρ/dt = 0, as proposed by L53, or the constant density case of S85. The atmosphere used in L53 or S85 does not allow the parcel to depart from hydrostatic equation during its adiabatic motions. The stronger the acceleration, the larger it departs from hydrostatic equilibrium, since \( \frac{dw}{dt}=-\frac{\partial p\hbox{'}}{\rho \partial z}-g\frac{\rho \hbox{'}}{\rho }. \)
The wind of a compressible air parcel can increase while the parcel rises with a cooling rate larger than adiabatic lapse rate. It means that extra-compressibility beyond the compression/expansion of hydrostatic–adiabatic process is crucial to the change of KE in the real atmosphere. The conventional Froude number only considers the conversion between the kinetic energy and potential energy as discussed in Eqs. (19) and (20) and is not definitive in the real atmosphere.
As discussed in Sun (2013), the zone of the weak (or reverse) winds in the mid-level (5 km ~ 10 km) creates a new blocking as an artificial steep mountain for the westerly flow in z = 7 ~ 8 km. The flow moves over and creates strong winds on the lee side of this blocking. Combining a strong wind passing over the zone of weak-wind barrier and that exiting from the upper part of the hydraulic jump, the westerly wind reaches more than 60 m s^{−1} in z ~ 8.2 km and x ~ 340 km. We can also see that the wind comes from z ≤ 8.2 km from the west and from the lower layer through the hydrostatic jump. Therefore, the increase of kinetic energy does not come from the conversion of potential energy, as discussed previously. The slanting strips of strong and weak (or reverse) westerly winds in z > 10 km resemble the propagating mountain waves. Because the air density decreases with height, the amplitude of mountain waves increase with height in the upper layer.
Case 2: Observed x-component wind and temperature of 11 January 1972 in Boulder are used at x = 0.
We can also identify the properties of the air parcel originating at 2A* (x = 160 km, z = 582.9 m) with B = 278,039 m^{2} s^{−2}, θ = 289.3 K, T = 271.10 K, and U = 2.18 m s^{−1}, which reaches the mountain top at 2B* (x = 320 km, z = 2061. m), where B = 278,039 m^{2} s^{−2}, θ = 289.3 K, T = 256.52 K, and U = 18.22 m s^{−1}. Again, \( {c}_p\left({T}_{\mathrm{A}*,\mathrm{B}*}^{\mathrm{ad}}-{T}_{\mathrm{B}*}\right) \) = 155.6 m^{2} s^{−2} is also close to KE_{B*} − KE_{A*} = 163.7 m^{2} s^{−2} shown in the rows of 2A* and 2B* of Table 1. The situation is similar to the previous case, even though the temperature and wind at x = 0 are height-dependent. Rows 2A*–2B* of Table 1 also show that θ remains nearly constant along a constant B-line, but the density changes considerably as discussed in case 1.
It is also notable that the pressure of the parcel is lower than the surrounding pressure at the same height (Fig. 3a, b). The contour of B = 2,790,000 m^{2} s^{−2} (Fig. 3a, b) shows that a warm parcel with a weak wind in the lower layer in the upstream rises to the mountain top while its temperature decreases beyond adiabatic lapse rate and the wind increases. Fig. 3a, b also shows that the region of strong downslope wind on the lee side is cooler than its surroundings. As discussed previously, the strong downslope wind originates from a relatively low level as in cases 1 and 2. The change of KE depends on \( {c}_p\left({T}_{i,f}^{\mathrm{ad}}-{T}_f\right) \) instead of the vertical displacement of gΔz. The source region of downslope wind around 2 km (Fig. 3b) is higher than in case 1 because of a strong wind shear at x = 0 in case 2.
Figure 3c and Table 1 show that the contours of θ (dashed black lines), streamlines, ρ (shaded color), and B _{L} (thick white line) based on ρ = ρ _{ i } (z, x = 0, t = 0) of Eq. (11a). The contours of B _{L} and density are parallel, but they intercept isentropic lines and streamlines near the mountain. This indicates that parcels at the mountain peak cannot follow a constant B _{L} to 2C (x = 340 km, z = 562.3 m). Similarly, the contours of B _{S} based on a constant density (ρ = 1 kg m^{−3}) of Eq. (11b) also intercept constant isentropic lines and streamlines (not shown); therefore, a parcel cannot follow B _{S} lines either.
Case 3: At x = 0, the observed x-component wind of 11 January 1972 in Boulder is used, but β = 3.5 K km^{−1} for z < 12 km; β = 0.7 K km^{−1} for z > 12 km.
Case 4. It is the same as case 2, except on a nonslip surface.
Conclusions
The Bernoulli equation is applied to an air parcel that originates from a low level at the inflow region, speeds up as it moves adiabatically over a mountain, then descends on the lee side and forms a strong downslope wind. Excess compressibility of the atmosphere beyond hydrostatic–adiabatic process allows the air parcel to depart from hydrostatic equilibrium, resulting in a change in kinetic energy (i.e., wind speed) which comes from changes in enthalpy. Numerical simulations confirm that potential temperature remains almost constant but temperature, density, and pressure vary considerably along constant Bernoulli lines. The mechanism described here does not appear in the incompressible, quasi-hydrostatic fluids used by L53 or S85. The results also suggest that the conventional Froude number, defined as the ratio of kinetic energy to the potential energy in the atmosphere, is not a good indicator for determining whether an air parcel can move over a mountain, except if the vertical motion is weak and the process is near hydrostatic equilibrium.
Declarations
Acknowledgements
We sincerely thank Prof. Y. L. Lin for the many useful comments and the reviewers for their comments, as well as Drs. W. R. Hsu, M. Shieh, B. MacCall, T. Oh, and S. H. Chen for their contributions to the development of the National Taiwan University–Purdue University nonhydrostatic model. The computing facilities provided by Purdue University are also appreciated.
Authors’ Affiliations
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