Geoscience Letters

Official Journal of the Asia Oceania Geosciences Society (AOGS)

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Bernoulli equation and flow over a mountain

Geoscience LettersOfficial Journal of the Asia Oceania Geosciences Society (AOGS)20152:7

DOI: 10.1186/s40562-015-0024-1

Received: 30 December 2014

Accepted: 10 April 2015

Published: 9 June 2015


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.


Adiabatic Bernoulli equation Downslope wind Enthalpy Froude number Hydrostatic–adiabatic process


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.


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

The 2D nonhydrostatic equations for the dry, compressible atmosphere can be written as:
$$ \frac{\partial u}{\partial t}+u\frac{\partial u}{\partial x}+w\frac{\partial u}{\partial z}=-\frac{1}{\rho}\frac{\partial p}{\partial x}+{D}_u $$
$$ \frac{\partial w}{\partial t}+u\frac{\partial w}{\partial x}+w\frac{\partial w}{\partial z}=-\frac{1}{\rho}\frac{\partial p}{\partial z}-g+{D}_w $$
$$ \frac{\partial \theta }{\partial t}+u\frac{\partial \theta }{\partial x}+w\frac{\partial \theta }{\partial z}={D}_{\theta } $$
$$ \frac{\partial \rho }{\partial t}=-\left(\frac{\partial \rho u}{\partial x}+\frac{\partial \rho w}{\partial z}\right) $$
$$ p=\rho RT $$
$$ \theta =T{\left(\frac{p_o}{p}\right)}^{R/{c}_p} $$
where u and w are the x- and z-components of the wind; p is the pressure; θ is the potential temperature; T is the temperature; ρ is the density; R is the gas constant; c p is the specific heat at constant pressure; D u and D w are the momentum diffusions along the x- and z-directions; and D θ is the heat diffusion. Equations (1)–(2) can be combined and written compactly in vector form
$$ \frac{\partial \mathbf{V}}{\partial t}+\nabla \left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)+\left(\nabla \times \mathbf{V}\right)\times \mathbf{V}-\frac{\nabla p}{\rho }-\mathbf{g}+\mathbf{D} $$
where V = (u, w). If we define the displacement by d r = (dx, dz) = V dt and integrate (7) from the initial state i to the final state f:
$$ {\displaystyle \underset{i}{\overset{f}{\int }}\left(\frac{\partial \mathbf{V}}{\partial t}+\nabla \left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)+\left(\nabla \times \mathbf{V}\right)\times \mathbf{V}-\frac{\nabla p}{\rho }+\mathbf{g}-\mathbf{D}\right)\bullet d\mathbf{r}}=0 $$

Because ( × V) × V is orthogonal to d r, ( × V) × V • d r = 0.

Thus, for a steady, inviscid flow, the Bernoulli equation becomes:
$$ \left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)\left|\begin{array}{c}\hfill {}^f\hfill \\ {}\hfill {}_i\hfill \end{array}+{\displaystyle \underset{i}{\overset{f}{\int }}\frac{dp}{\rho }+gz\left|{}_{{}_{{}_i}}^{{}^f}=0.\right.}\right. $$
Because in adiabatic process \( {c}_pdT-\frac{dp}{\rho }=0, \) Eq. (9a) becomes:
$$ {\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_f+{C}_p{T}_f+g{z}_f={\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_i+{C}_p{T}_i+g{z}_i=B\;\left(\mathrm{Bernoulli}\kern0.5em \mathrm{function}\right) $$
Equation (9a) has been discussed in Clancy (1975). Bernoulli function remains constant along a streamline. From Eq. (9b), we can obtain
$$ d\left[\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)+{c}_pT+gz\right]=d\left(\mathrm{K}\mathrm{E}\right)+{c}_pdT+gdz=0 $$

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).

We also define
$$ {B}_L\equiv \left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)+\frac{p}{\rho_{\mathrm{i}}\left(z,x=0\right)}+gz $$
$$ {B}_s\equiv \left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)+\frac{p}{\rho_c}+gz $$

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.

Here, we will define a hydrostatic–adiabatic process as an air parcel moves adiabatically from z i to z f and follows the hydrostatic equation (i.e., dw/dt ~ 0). The change of pressure with height in a hydrostatic–adiabatic process can be derived
$$ dp=-\rho gdz=-{\rho}_i{\left(\frac{p}{p_i}\right)}^{c_v/{c}_p}gdz $$
$$ {\displaystyle \underset{z_i}{\overset{z_f}{\int }}gdz}=g\left({z}_f-{z}_i\right)=g\varDelta z=-\frac{p_i^{c_v/{c}_p}}{\rho_i}{\displaystyle \underset{p_i}{\overset{p_f}{\int }}{p}^{-{c}_v/{c}_p}}dp={c}_p\left({T}_i-{T}_f\right) $$
The temperature lapse rate is:
$$ \beta =-\frac{T_i-{T}_f}{z_i-{z}_f}=\frac{g}{c_p}\equiv {\beta}_{\mathrm{ad}} $$

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.

Substituting (13) into Eq. (9b), we obtain
$$ {\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_f={\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_i $$
which confirms that the kinetic energy remains constant in a hydrostatic–adiabatic process. When a parcel has a large vertical velocity, it usually does not satisfy hydrostatic equilibrium. Hence T f is different from (T i  − β adΔz), Eq. (9b) can be written as:
$$ \begin{array}{l}{\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_f-{\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_i={c}_p{T}_i-{c}_p{T}_f+g{z}_i-g{z}_f={c}_p\left[{T}_i-\frac{g}{c_p}\left({z}_f-{z}_i\right)\right]-{c}_p{T}_f\\ {}={c}_p\left[{T}_i-{\beta}_{\mathrm{ad}}\varDelta z\right]-{c}_p{T}_f={c}_p{T}_{i,f}^{\mathrm{ad}}-{c}_p{T}_f={c}_p\left({T}_{i,f}^{\mathrm{ad}}-{T}_f\right)\end{array} $$
where the temperature \( {T}_{i,f}^{\mathrm{ad}}={T}_i-{\beta}_{\mathrm{ad}}\varDelta z, \) is the temperature of an “artificial” air parcel moves from i to f following the adiabatic lapse rate β ad in a hydrostatic–adiabatic process, which is different from the simulated temperature T f . Equation (16) also implies that the change of kinetic energy comes from the enthalpy difference, \( {c}_p\left({T}_{i,f}^{\mathrm{ad}}-{T}_f\right) \). The temperatures T f and \( {T}_{i,f}^{\mathrm{ad}} \) will be presented in Table 1. The adiabatic lapse rate can also be derived from /dz = 0 and hydrostatic equation. Hence, adiabatic lapse rate β ad is a warming/cooling rate in a hydrostatic–adiabatic process without changing the kinetic energy (KE) according to Eqs. (15) and (16).
Table 1

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 (mzs −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 (mZ 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 (mZ s−2)























































































































































































































*indicates parcel trajectory at the inflow region and at mountain peak

If the hydrostatic equation is applied to Eqs. (11a) and (11b), the KE of the parcel keeps its initial value because
$$ dp = -g{p}_cdz\ or\ dp = -g{p}_idz. $$
If the pressure of an air parcel automatically adjusts to its environment \( \left(p=\overline{p}\right), \) which is in hydrostatic equilibrium, during adiabatic motion (i.e., the parcel method in meteorology), the parcel temperature from i to f can be calculated by
$$ {T}_f={T}_i{\left(\frac{p_f}{p_i}\right)}^{R/{c}_p}={T}_i{\left(\frac{{\overline{p}}_f}{p_i}\right)}^{R/{c}_p}={T}_i{\left[{\left(\frac{T_i-\overline{\beta}\varDelta z}{T_i}\right)}^{\frac{g}{\overline{\beta}R}}\right]}^{R/{c}_p}={T}_i{\left(\frac{T_i-\overline{\beta}\varDelta z}{T_i}\right)}^{\frac{g}{\overline{\beta}{c}_p}} $$
where Δz = z f  − z i , and the lapse rate of the environment (with over bar) \( \overline{\beta}=-\frac{d\overline{T}}{dz}, \) and \( d\overline{p}=-\overline{\rho}gdz=-\frac{\overline{p}gdz}{R\overline{T}}, \) or \( d \ln \overline{p}=-\frac{g}{R\overline{\beta}}d \ln \left({T}_i-\overline{\beta}z\right) \). Equation (9b) becomes
$$ \begin{array}{l}{\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_i-{\left(\frac{\mathbf{V}\bullet \mathbf{V}}{2}\right)}_f={c}_p{T}_i\left[{\left(\frac{T_i-\overline{\beta}\varDelta z}{T_i}\right)}^{\frac{g}{\overline{\beta}{c}_p}}-1\right]+g\varDelta z\\ {}={c}_p{T}_i\left[{\left(1-\frac{\overline{\beta}\varDelta z}{T_i}\right)}^{\frac{g}{\overline{\beta}{c}_p}}-1\right]+g\varDelta z\\ {}={c}_p{T}_i\left\{\left[1-\frac{g}{\overline{\beta}{c}_p}\frac{\overline{\beta}\varDelta z}{T_i}+\frac{g}{2\overline{\beta}{c}_p}\left(\frac{g}{\overline{\beta}{c}_p}-1\right){\left(\frac{\overline{\beta}\varDelta z}{T_i}\right)}^2-\dots \right]-1\right\}+g\varDelta z\\ {}=\frac{c_p{T}_ig}{2\overline{\beta}{c}_p}\left(\frac{g}{\overline{\beta}{c}_p}-1\right){\left(\frac{\overline{\beta}\varDelta z}{T_i}\right)}^2-\dots =\frac{g}{2}\left(\frac{g}{c_p}-\overline{\beta}\right)\left(\frac{\varDelta {z}^2}{T_i}\right)-\dots =\frac{1}{2}\frac{g}{\overline{\theta}}\frac{d\overline{\theta}}{dz}\varDelta {z}^2-\dots \\ {}\end{array} $$
$$ \frac{g}{\theta}\frac{d\overline{\theta}}{dz}\varDelta {z}^2={N}^2\varDelta {z}^2={\left(\mathbf{V}\bullet \mathbf{V}\right)}_i-{\left(\mathbf{V}\bullet \mathbf{V}\right)}_f=2{\mathrm{KE}}_i-2{\mathrm{KE}}_f $$

where N is the Brunt–Väisälä frequency.

Equation (19) shows that 2KE i  − 2KE f can be converted to potential energy N 2Δz 2 in a stable atmosphere. Let us define Rat:
$$ \mathrm{Rat}=\frac{\sqrt{2{\mathrm{KE}}_i-2{\mathrm{KE}}_f}}{N\varDelta z} $$
If KE f  = 0 and Δz = mountain height h, and \( 2{\mathrm{KE}}_i=\mathbf{V}\bullet \mathbf{V}={U}_i^2, \) where U i is the characteristic horizontal velocity at the inflow region, then Rat is identical to the conventional Froude number in meteorology \( \mathrm{F}\mathrm{r}=\frac{U_i}{Nh}, \) which is related to the ratio of the kinetic energy change to the potential energy change. The Froude number can also be derived for Boussinesq fluid which experiences a hydraulic jump over an obstacle of height h:
$$ \mathrm{F}\mathrm{r}=\frac{U_i}{\sqrt{g\hbox{'}h}}=\frac{U_i}{\sqrt{g\frac{\theta \hbox{'}}{\theta }h}}=\frac{U_i}{\sqrt{gh\frac{\left({\theta}_i\frac{d\overline{\theta}}{dz}h\right)-{\theta}_i}{\theta }}}=\frac{U_i}{\sqrt{\frac{g}{\theta}\frac{d\overline{\theta}}{dz}{h}^2}}=\frac{U_i}{Nh}. $$

where g’ = ’/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.

For a large mountain about 10-km wide (a ~ 10 km), the mountain waves may be considered as hydrostatic nonrotating waves in linear theory (Gill 1982). The constant phase lines are tilted upstream with height, thus producing a high pressure on the windward slope and a low pressure on the lee slope. The flow decelerates over the windward slope and accelerates over the lee slope. The ground level pressure perturbation and wind vanish at the peak (Gill 1982; Lin 2007). The linearized equations also show that the decrease of the wind on the windward slope is equal to the increase of wind on the lee side. However, they are different from the nonlinear model simulations, in which the increase of wind on the lee slope is much larger than the decrease on the windward slope; the positive wind perturbation extends to the mountain peak, as shown in Durran (1986), Hsu and Sun (2001), etc. But, it was mostly ignored because the conventional theory states that the change of kinetic energy comes from the decrease of potential energy. The patterns of the surface wind and pressure simulated from nonlinear models with a = 10 km are close to the pattern of the linear, nonhydrostatic waves with a ~ 1 km than the hydrostatic waves discussed in Queney (1948), Gill (1982), etc. The increase of U at the peak further reduces the pressure according to Bernoulli equation and results in sucking more air from the lower layer in the upstream. Because the pressure p f is lower than the pressure on the upstream region at the same height, p env, according to (6), we obtain
$$ {T}_f=\theta {\left(\frac{p_f}{p_o}\right)}^{R/{c}_p}<{T}_{\mathrm{env}}=\theta {\left(\frac{p_{\mathrm{env}}}{p_o}\right)}^{R/{c}_p}={T}_{i,f}^{\mathrm{ad}} $$

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.

From (5), we may obtain
$$ d \ln p=d \ln \rho +d \ln T,\ \mathrm{or}\ \frac{p\hbox{'}}{p}=\frac{\rho \hbox{'}}{\rho }+\frac{T\hbox{'}}{T} $$
For an adiabatic process, from (6), we obtain
$$ d \ln T=d \ln \theta +\frac{R}{c_p}d \ln p,\ \mathrm{or}\ \frac{T\hbox{'}}{T}=\frac{R}{c_p}\frac{p\hbox{'}}{p} $$
If we define \( T\hbox{'}={T}_f-{T}_{i,f}^{\mathrm{ad}} \), we can obtain
$$ \frac{p\hbox{'}}{p}=\frac{C_p}{R}\frac{T\hbox{'}}{T},\ \mathrm{and}\ \frac{\rho \hbox{'}}{\rho }=\frac{C_v}{R}\frac{T\hbox{'}}{T}, $$

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.

The Arakawa C grids are applied in the terrain following the σ-coordinate, which is defined as:
$$ \sigma =\frac{p_0(z)-{p}_0\left({z}_{\mathrm{top}}\right)}{p_0\left({z}_{\mathrm{surface}}\right)-{p}_0\left({z}_{\mathrm{top}}\right)}, $$

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.

Figure 1a shows the simulated x-component wind (indicated by a shaded color), potential temperature θ (dashed black lines), Bernoulli function B (thick white line), streamlines (thin black line), and pressure p (thin white line) at t = 6 h, when the flows are almost steady except in the highly turbulent regions. Fig. 1b is the same as Fig. 1a, except that the shaded colors indicate temperature. The contours of B, θ, and streamlines are almost parallel before flows reach the highly turbulent areas on the lee side, indicating that the flow is nearly steady, adiabatic, and inviscid, even though weak smoothing and a turbulence parameterization are present in the model. The contours of B or θ are thus approximately trajectories, except inside areas of high turbulence.
Fig. 1

a Simulated U (shaded color), B (thick white lines), θ (dashed black lines), p (thin white lines), and streamlines at t = 6 h integration for case 1. b Same as Fig. 1a except that the shaded color represents temperature T

We can follow the trajectory of an air parcel along B = 280,000 m2 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, KEB − KEA = 445.7 m2 s−2, and the difference in enthalpy \( {c}_p\left({T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}-{T}_{\mathrm{B}}\right) \) = 487.9 m2 s−2 at 1B. The difference of kinetic energy between 1B and 1C is 2263 m2 s−2 and \( {c}_p\left({T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}-{T}_{\mathrm{C}}\right) \) is 2272 m2 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 m2 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 m2 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 m2 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 m2 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 m2 s−2 and is also very close to \( {c}_p\left({T}_{\mathrm{A}*,\mathrm{B}*}^{\mathrm{ad}}-{T}_{\mathrm{B}*}\right) \) = 250.0 m2 s−2 at 1B* according to Eq. (16).

Along B = 280,000 m2 s−2 at 1A, 1B, and 1C, θ remains around 291.1 K, but the density changes considerably following the motion (i.e., /dt ≠ 0); density also changes noticeably but θ remains near 286.9 K along B = 276,007 m2 s−2 at 1A* and B*. This differs significantly from /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.

This case has been studied intensively, as discussed in Sun (2013) and papers quoted in Background and in Klemp and Lilly (1975), Lilly (1978), Clark and Peltier (1984), Durran (1986), Doyle et al. (2000), Hsu and Sun (2001), Sun and Hsu (2005), Lin (2007), etc. Fig. 2a, b shows the observed wind and potential temperature as functions of height at the inflow region. The shaded colors in Fig. 3a, b, c show the simulated wind, temperature, and density, respectively, at t = 6 h. The contours of B (thick white line), θ (dashed black lines), and the streamlines are almost parallel before the flow becomes turbulent, similar to case 1. Bernoulli B = 279,890 m2 s−2 at 2C (x = 340 km, z = 562.3 m), the location of a severe downslope wind on the lee side, where U = 65.61 m s−1, θ = 291.3 K, T = 271.01 K, and ρ = 0.9987 kg m−3. The contour B = 279,890 m2 s−2 can be traced back to 2B (x = 320 km, z = 2227 m) over the mountain peak, where U = 22.94 m s−1, θ = 291.3 K, T = 256.65 K, and ρ = 0.8715 kg m−3, and 2A (x = 160 km, z = 1123 m) in the upstream where U = 4.037 m s−1, θ = 291.3 K, T = 267.67 K, and ρ = 0.9685 kg m−3. Rows 2A, 2B, and 2C in Table 1 show that the temperature at 2B, T B = 256.65 K, is cooler than \( {T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}} \) = 256.90 K, and T C = 271.01 K is less than \( {T}_{\mathrm{B}\operatorname{},\mathrm{C}}^{\mathrm{ad}} \) = 272.90 K at 2C. The large increase in KE between 2B and 2C (KEC − KEB = 1892 m2 s−2) is consistent with \( {c}_p\left({T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}-{T}_{\mathrm{C}}\right) \) = 1898.0 m2 s−2 due to a large cooling (1.89 K) of the air parcel while it ascends/descends adiabatically. It is noted that the extra cooling also accompanies the pressure and density decreases compared to hydrostatic–adiabatic process in the area of severe downslope wind on the lee side (Fig. 2a, b).
Fig. 2

a θ (z) at inflow for case 2. b U (z) at inflow for case 2

Fig. 3

a Same as Fig. 1a except for case 2. b Same as Fig. 1b except for case 2. c ρ (shaded color), θ (dashed black lines), p (thin white lines), streamlines, and B L (thick white lines), based on ρ i in Eq. (11a) at t = 6 h for case 2

We can also identify the properties of the air parcel originating at 2A* (x = 160 km, z = 582.9 m) with B = 278,039 m2 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 m2 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 m2 s−2 is also close to KEB* − KEA* = 163.7 m2 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 m2 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.

The simulated wind (shaded colors) at t = 6 h (Fig. 4) reveals that the downslope wind (U = 23.23 m s−1) at 3C (x = 353 km, z = 305.1 m; row 3C in Table 1) is much weaker than the U = 65.6 m s−1 of case 2 or 74 m s−1 of case 1. A stable stratification and a weak wind in the low layer cause the flow to move over the mountain in close to hydrostatic equilibrium (i.e., dw/dt ≈ 0). At 3A (x = 160 km, z = 531.3 m), U = 8.159 m s−1 is slightly less than U = 10.71 m s−1 at 3B (x = 320 km, z = 2139 m), and T B = 253.84 K is slightly less than \( {T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}=253.86\mathrm{K}. \) KEB − KEA = 24.16 m2 s−2 is very close to \( {c}_p\left({T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}-{T}_{\mathrm{B}}\right) \) = 17.07 m2 s−2. The increase of KE at 3B comes from the decrease of enthalpy. At 3C, T C = 271.52 K is also slightly less than \( {T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}=271.74\mathrm{K}, \) and \( {c}_p\left({T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}-{T}_{\mathrm{C}}\right) \) = 220.9 m2 s−2 is close to KEC − KEB = 212.5 m2 s−2. This is consistent with the Bernoulli equation and also confirms that if \( {T}_{i,f}^{\mathrm{ad}}={T}_i-{\beta}_{\mathrm{ad}}\varDelta z\approx {T}_f, \) we will have KE f  ≈ KE i .
Fig. 4

Same as Fig. 1a except for case 3

Case 4. It is the same as case 2, except on a nonslip surface.

Since a free-slip surface is unrealistic, we examine the validity of the Bernoulli equation over a nonslip surface, which avoids the propagation of the hydraulic jump obtained on a free-slip surface. The simulated θ and B lines at t = 6 h deform drastically due to the effect of surface friction (Fig. 5). However, θ and B lines at 500 m or more above the ground are not affected by surface friction. Table 1 shows that the contour of B = 283,597 m2 s−2 comes from 4A (x = 160 km, z = 2870. m) with U = 18.55 m s−1 and θ = 295.7 K and reaches 4B (x = 320 km, z = 3149 m) over the mountain peak with U = 24.16 m s−1 and θ = 295.7 K. The change of kinetic energy, KEB − KEA = 120.5 m2 s−2 is very close to \( {c}_p\left({T}_{\mathrm{A},\mathrm{B}}^{\mathrm{ad}}-{T}_{\mathrm{B}}\right) \) = 119.5 m2 s−2. After passing over the mountain peak, the flow descends and creates a strong downslope wind U = 38.19 m s−1 and θ = 295.6 K at 4C (x = 332 km, z = 1087.08 m). KEC − KEB = 446.7 m2 s−2 and \( {c}_p\left({T}_{\mathrm{B},\mathrm{C}}^{\mathrm{ad}}-{T}_{\mathrm{C}}\right) \) = 436.7 m2 s−2. These are in good agreement because they are derived from a very large value of B (=283,597 m2 s−2). Above the surface friction layer, lines of θ, B, and streamlines are nearly parallel. The potential temperature is almost conserved along B = 283,597 m2 s−2 as well. The wind speed increases while the parcel moves over the mountain top at x = 320 km, along B = 283,597 m2 s−2. However, the contours of B ≤ 281,000 m2 s−2 deform drastically when they approach the mountain. They are also quite irregular in the areas of high turbulence on the lee side, where the flow becomes unsteady. The strong downslope wind comes from a layer which is above the influence of surface friction. Overall, the downslope wind is much weaker than in case 2. As discussed in Sun (2013), the severe downslope wind can be enhanced and maintained by the convergence of the geostrophic-unbalanced, northwesterly upper-level-jet due to geostrophic adjustment. The simulated wind here is much weaker than those in Sun (2013), because neither the Coriolis force nor the geostrophic-unbalanced upper-level jet is included here. For more details, the reader is referred to Sun (2013).
Fig. 5

Same as Fig. 1a except for case 4


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.



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

Department of Earth, Atmospheric and Planetary Sciences, Purdue University
Department of Atmospheric Sciences, National Central University
Hydrospheric Atmospheric Research Center (HyARC), Nagoya University
Woods Hole Oceanographic Institution
Present address: Naval Undersea Warfare Center


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