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7c3bfa9 | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 199 200 201 202 203 204 205 206 207 208 209 210 211 212 213 214 215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232 233 234 235 236 237 238 239 240 241 242 243 244 245 246 247 248 249 250 251 252 253 254 255 256 257 258 259 260 261 262 263 264 265 266 267 268 269 270 271 272 273 274 275 276 277 278 279 280 281 282 283 284 285 286 287 288 289 290 291 292 293 294 295 296 297 298 299 300 301 302 303 304 305 306 307 308 309 310 311 312 313 314 315 316 317 318 319 320 321 322 323 324 325 326 327 328 329 330 331 332 333 334 335 336 337 338 339 340 341 342 343 344 345 346 347 348 349 350 351 352 353 354 355 356 357 358 359 360 361 362 363 364 365 366 367 368 369 370 371 372 373 374 375 376 377 378 379 380 381 382 383 384 385 386 387 388 389 390 391 392 393 394 395 396 397 398 399 400 401 402 403 404 405 406 407 408 409 410 411 412 413 414 415 416 417 418 419 420 421 422 423 424 425 426 427 428 429 430 431 432 433 434 435 436 437 438 439 440 441 442 | """Pure-Python reference implementation of the mountain-wave solver.
This module is a direct transcription of the MATLAB routines ``tlwplot.m``
and ``stream.m`` written by Dr. Robert E. (Bob) Hart in 1995 as a Penn
State Meteo 574 seminar project (see
https://moe.met.fsu.edu/~rhart/mtnwave.html). The two-layer routine here
mirrors Hart's MATLAB code line-for-line (reformulated in NumPy); the
multi-layer routine is a natural generalization using the same Fourier +
transfer-matrix scheme.
It exists for two reasons:
1. It's the fallback when the Rust extension isn't built.
2. It's the reference used by ``validate.py`` to confirm the Rust core
produces bit-similar results.
The multi-layer solver implements the same transfer-matrix scheme as the
Rust version so they can be compared.
"""
from __future__ import annotations
import math
import numpy as np
G = 9.80665
# ---------------------------------------------------------------------------
# Two-layer analytic solver (port of tlwplot.m)
# ---------------------------------------------------------------------------
def compute_two_layer(
l_upper: float,
l_lower: float,
u: float,
h: float,
a: float,
ho: float,
xdom: float,
zdom: float,
mink: float,
maxk: float,
npts: int = 100,
):
"""Return ``(x, z, w, u_prime)`` for flow over a witch-of-Agnesi mountain.
Arrays match the MATLAB conventions: ``x`` has shape ``(npts + 1,)``,
``z`` has shape ``(npts + 1,)``, and both ``w`` and ``u_prime`` have
shape ``(z.size, x.size)`` indexed as ``[z_index, x_index]``.
``u_prime`` is the wave-induced horizontal wind perturbation, obtained
from linearized continuity ``∂u'/∂x + ∂w/∂z = 0``. Per wavenumber,
``u'_k = −(i/k) · ∂ŵ_k/∂z``; we analytically differentiate the two-layer
eigenfunctions (``A e^{−n z}`` above the interface, ``C e^{i m z} +
D e^{−i m z}`` below) and accumulate the same trapezoidal k-integration
used for ``w``.
"""
dk = 0.367 / a
nk = max(1, int((maxk - mink) // dk))
minx = -0.25 * xdom
maxx = 0.75 * xdom
dx = (maxx - minx) / npts
dz = zdom / npts
x = minx + dx * np.arange(npts + 1)
z = dz * np.arange(npts + 1)
X, Z = np.meshgrid(x, z) # shape (npts+1, npts+1), Z[i, j] varies along i
matrix1 = np.zeros_like(X, dtype=complex)
matrix3 = np.zeros_like(X, dtype=complex)
matrix1_u = np.zeros_like(X, dtype=complex)
matrix3_u = np.zeros_like(X, dtype=complex)
ht = 0.0
for kloop in range(nk + 1):
kk = mink + dk * kloop
m = np.sqrt(complex(l_lower ** 2 - kk ** 2))
n = np.sqrt(complex(kk ** 2 - l_upper ** 2))
denom = m + 1j * n
if abs(denom) < 1e-300:
r = complex(9e99, 0.0)
else:
r = (m - 1j * n) / denom
R = r * np.exp(2j * m * h)
A = (1 + r) * np.exp(h * n + 1j * h * m) / (1 + R)
C = 1.0 / (1 + R)
D = R * C
ksign = abs(kk)
hs = np.pi * a * ho * np.exp(-a * ksign)
ht += np.pi * dk * a * np.exp(-a * ksign) if kloop > 0 else 0.0
above = A * np.exp(-Z * n) * (Z > h)
below = (C * np.exp(1j * Z * m) + D * np.exp(-1j * Z * m)) * (Z <= h)
matrix2 = (-1j * kk * hs * u * (above + below)) * np.exp(-1j * X * kk)
# Analytic z-derivative of the eigenfunctions (the two branches are
# continuous at z=h by construction, so the jump in the step factor
# contributes nothing to the derivative inside each region).
dabove = (-n) * A * np.exp(-Z * n) * (Z > h)
dbelow = (1j * m) * (C * np.exp(1j * Z * m) - D * np.exp(-1j * Z * m)) * (Z <= h)
# u'_k(x, z) = (-i/k) · ∂ŵ_k/∂z. Combining the −ik factor baked into
# matrix2's ŵ formula with the −i/k in front yields −hs·U·∂(above+
# below)/∂z. This removes the apparent 1/k singularity at k=0 — the
# result is analytic there — and avoids division edge cases.
matrix2_u = (-hs * u) * (dabove + dbelow) * np.exp(-1j * X * kk)
if kloop > 0:
matrix3 += 0.5 * (matrix1 + matrix2) * dk
matrix3_u += 0.5 * (matrix1_u + matrix2_u) * dk
matrix1 = matrix2
matrix1_u = matrix2_u
if ht == 0.0:
ht = 1.0
w = np.real(matrix3 / ht)
u_prime = np.real(matrix3_u / ht)
return x, z, w, u_prime
# ---------------------------------------------------------------------------
# Multi-layer profile solver
# ---------------------------------------------------------------------------
# Minimum |U| used in the Scorer-parameter denominator. In pure linear
# theory, U(z) = 0 is a critical level where l² = N²/U² − (U″/U) is
# singular; linear Scorer/Taylor-Goldstein cannot honestly solve across
# such a level. In a teaching tool we *want* students to be able to set
# up a wind-reversal profile and see what happens away from the critical
# level rather than have the whole solve NaN out. We clamp |U| to this
# floor (preserving sign) when evaluating the Scorer coefficients. Away
# from U≈0 this is a no-op; within ±0.5 m/s it caps l² at a large but
# finite value and the UI emits a "critical level detected" warning so
# nobody is misled into treating the capped zone as physical.
U_FLOOR_SCORER = 0.5 # m/s
def _u_clamped_for_scorer(uu: float) -> float:
"""Return ``uu`` with ``|uu|`` lifted to ``U_FLOOR_SCORER``; sign preserved."""
if uu >= 0.0:
return max(uu, U_FLOOR_SCORER)
return min(uu, -U_FLOOR_SCORER)
def scorer_from_profile(z_profile, u_profile, theta_profile):
"""Return Scorer parameter L^2(z) computed from profile data.
Handles wind reversals (sign changes in ``u_profile``) by clamping the
magnitude of ``U`` at ``U_FLOOR_SCORER`` when it evaluates the
``N²/U² − U″/U`` combination. This keeps the solver numerically
well-behaved across a critical level (``U = 0``) at the cost of a
physically sharp feature there — see the ``critical_levels`` helper
below for the companion diagnostic surfaced in the UI.
"""
z = np.asarray(z_profile, dtype=float)
u = np.asarray(u_profile, dtype=float)
theta = np.asarray(theta_profile, dtype=float)
n = z.size
l2 = np.zeros(n)
for i in range(n):
if i == 0:
dthdz = (theta[1] - theta[0]) / (z[1] - z[0])
if n >= 3:
h1 = z[1] - z[0]
h2 = z[2] - z[1]
d2u = 2.0 * (u[2] * h1 - u[1] * (h1 + h2) + u[0] * h2) / (h1 * h2 * (h1 + h2))
else:
d2u = 0.0
elif i == n - 1:
dthdz = (theta[-1] - theta[-2]) / (z[-1] - z[-2])
if n >= 3:
h1 = z[-2] - z[-3]
h2 = z[-1] - z[-2]
d2u = 2.0 * (u[-1] * h1 - u[-2] * (h1 + h2) + u[-3] * h2) / (h1 * h2 * (h1 + h2))
else:
d2u = 0.0
else:
h1 = z[i] - z[i - 1]
h2 = z[i + 1] - z[i]
dthdz = (
theta[i + 1] * h1 ** 2
- theta[i - 1] * h2 ** 2
+ theta[i] * (h2 ** 2 - h1 ** 2)
) / (h1 * h2 * (h1 + h2))
d2u = 2.0 * (u[i + 1] * h1 - u[i] * (h1 + h2) + u[i - 1] * h2) / (h1 * h2 * (h1 + h2))
n2 = (G / theta[i]) * dthdz
uu = _u_clamped_for_scorer(u[i])
l2[i] = n2 / uu ** 2 - d2u / uu
return l2
def critical_levels(z_profile, u_profile):
"""Return heights (m) where ``u_profile`` crosses zero, linearly interpolated.
A "critical level" for steady, 2-D, horizontally uniform linear mountain
waves is a height where the mean flow vanishes (``U = 0``). Linear
Scorer/Taylor-Goldstein theory is singular there — wave energy is
absorbed rather than propagated (Booker & Bretherton 1967) — so any
result the solver returns *near* a critical level should be read as
"this is where the linear model breaks down," not as a prediction.
Caller (the Dash UI) surfaces the returned heights in a diagnostics
badge so students can see where their profile is violating the
assumptions of the model.
"""
z = np.asarray(z_profile, dtype=float)
u = np.asarray(u_profile, dtype=float)
heights = []
for i in range(1, z.size):
u_prev, u_curr = u[i - 1], u[i]
# Treat exact zeros as crossings at that sample.
if u_curr == 0.0:
heights.append(float(z[i]))
continue
if u_prev == 0.0:
# Already recorded by the previous iteration's "u_curr == 0" branch.
continue
if (u_prev > 0.0 and u_curr < 0.0) or (u_prev < 0.0 and u_curr > 0.0):
# Linear interp to the zero crossing.
t = u_prev / (u_prev - u_curr)
heights.append(float(z[i - 1] + t * (z[i] - z[i - 1])))
return heights
def compute_from_profile(
z_profile,
u_profile,
theta_profile,
a: float,
ho: float,
xdom: float,
zdom: float,
mink: float,
maxk: float,
npts: int = 100,
):
"""Arbitrary u(z)/theta(z) mountain-wave solver using transfer matrices.
Returns ``(x, z, w, u_prime)``. The atmosphere is split into
piecewise-constant L² layers centered on the profile points. Inside
each layer the wave-transform equation reduces to an exponential
ansatz; continuity of ŵ and ŵ' at interfaces plus a radiation / decay
condition aloft closes the system.
The wave-induced horizontal wind perturbation ``u_prime`` is obtained
in the same Fourier loop: for each wavenumber ``k ≠ 0`` we take the
analytic z-derivative of the per-layer ŵ basis (``σ_j · (−a_j
e^{−σ_j Δz} + b_j e^{+σ_j Δz})``) and multiply by ``−i/k`` from the
linearized continuity relation ``u'_k = −(i/k) · ∂ŵ_k/∂z``.
"""
zp = np.asarray(z_profile, dtype=float)
up = np.asarray(u_profile, dtype=float)
tp = np.asarray(theta_profile, dtype=float)
l2 = scorer_from_profile(zp, up, tp)
u_surface = float(up[0])
nlayers = zp.size
layer_bot = np.empty(nlayers)
layer_top = np.empty(nlayers)
for j in range(nlayers):
layer_bot[j] = 0.0 if j == 0 else 0.5 * (zp[j - 1] + zp[j])
layer_top[j] = np.inf if j == nlayers - 1 else 0.5 * (zp[j] + zp[j + 1])
dk = 0.367 / a
nk = max(1, int((maxk - mink) // dk))
nslab = nk + 1
minx = -0.25 * xdom
maxx = 0.75 * xdom
dx = (maxx - minx) / npts
dz = zdom / npts
x = minx + dx * np.arange(npts + 1)
z = dz * np.arange(npts + 1)
# Layer index for each vertical grid point
layer_of = np.zeros(z.size, dtype=int)
for j, zj in enumerate(z):
idx = nlayers - 1
for lj in range(nlayers):
if zj < layer_top[lj]:
idx = lj
break
layer_of[j] = idx
matrix1 = np.zeros((z.size, x.size), dtype=complex)
matrix3 = np.zeros((z.size, x.size), dtype=complex)
matrix1_u = np.zeros((z.size, x.size), dtype=complex)
matrix3_u = np.zeros((z.size, x.size), dtype=complex)
ht = 0.0
for kloop in range(nslab):
kk = mink + dk * kloop
ksign = abs(kk)
hs = np.pi * a * ho * np.exp(-a * ksign)
if kloop > 0:
ht += np.pi * dk * a * np.exp(-a * ksign)
if kk == 0.0:
# DC mode has no wave contribution; u' also vanishes here.
matrix2 = np.zeros_like(matrix1)
matrix2_u = np.zeros_like(matrix1)
else:
# Principal-branch sigma: in each layer, the "a" coefficient
# multiplies exp(-sigma*dz), which is always the outgoing /
# decaying branch when Im(sigma) >= 0.
sigma = np.empty(nlayers, dtype=complex)
for j in range(nlayers):
s = np.sqrt(complex(kk ** 2 - l2[j]))
if s.imag < 0:
s = -s
sigma[j] = s
aj = np.zeros(nlayers, dtype=complex)
bj = np.zeros(nlayers, dtype=complex)
aj[-1] = 1.0
bj[-1] = 0.0
for j in range(nlayers - 2, -1, -1):
dz_j = layer_top[j] - layer_bot[j]
e_minus = np.exp(-sigma[j] * dz_j)
e_plus = np.exp(sigma[j] * dz_j)
alpha = aj[j + 1] + bj[j + 1]
beta = -aj[j + 1] + bj[j + 1]
ratio = sigma[j + 1] / sigma[j]
aj[j] = 0.5 * (alpha - ratio * beta) * e_plus
bj[j] = 0.5 * (alpha + ratio * beta) * e_minus
w_surface = aj[0] + bj[0]
if abs(w_surface) < 1e-300:
amp = 0.0 + 0.0j
else:
amp = -1j * kk * u_surface * hs / w_surface
aj *= amp
bj *= amp
# Build ŵ and ∂ŵ/∂z on the vertical grid. The per-layer basis
# ŵ_j(z) = a_j e^{−σ_j Δz} + b_j e^{+σ_j Δz}
# differentiates cleanly to
# ∂ŵ_j/∂z = σ_j · (−a_j e^{−σ_j Δz} + b_j e^{+σ_j Δz})
# and the continuity relation gives u'_k = −(i/k) · ∂ŵ/∂z.
zfac = np.zeros(z.size, dtype=complex)
zfac_u = np.zeros(z.size, dtype=complex)
inv_ik = -1j / kk
for j in range(z.size):
lj = layer_of[j]
dz_l = z[j] - layer_bot[lj]
e_minus = np.exp(-sigma[lj] * dz_l)
e_plus = np.exp(sigma[lj] * dz_l)
zfac[j] = aj[lj] * e_minus + bj[lj] * e_plus
dwdz = sigma[lj] * (-aj[lj] * e_minus + bj[lj] * e_plus)
zfac_u[j] = inv_ik * dwdz
xfac = np.exp(-1j * x * kk)
matrix2 = np.outer(zfac, xfac)
matrix2_u = np.outer(zfac_u, xfac)
if kloop > 0:
matrix3 += 0.5 * (matrix1 + matrix2) * dk
matrix3_u += 0.5 * (matrix1_u + matrix2_u) * dk
matrix1 = matrix2
matrix1_u = matrix2_u
if ht == 0.0:
ht = 1.0
w = np.real(matrix3 / ht)
u_prime = np.real(matrix3_u / ht)
return x, z, w, u_prime
# ---------------------------------------------------------------------------
# Streamline tracer (port of stream.m)
# ---------------------------------------------------------------------------
def streamlines(x, z, u, w, num: int = 10):
"""Return ``num`` streamlines as ``[(xs, ys), ...]`` polylines.
``u`` may be a scalar (uniform mean flow, used for the two-layer solver)
or a 1-D array of length ``nz`` giving the mean wind at each render-grid
height. In linear wave theory the parcel displacement at height ``z₀`` is
``η(x, z₀) = (1/U(z₀)) · ∫ w(x', z₀) dx'``, so the time step used to
integrate along each streamline depends on the wind at that streamline's
height — not on the surface wind. Using a single scalar ``U_surface`` for
every streamline (as Hart's MATLAB ``stream.m`` did because the two-layer
case assumed uniform ``U``) over-amplifies upper streamlines whenever the
real profile has shear.
We guard against near-zero ``U(z₀)`` (which would blow up the tracer) with
a 0.1 m/s floor — a parcel literally at rest cannot trace a linear
streamline in this framework, so we just freeze it there.
"""
x = np.asarray(x)
z = np.asarray(z)
w = np.asarray(w)
nx = x.size
nz = z.size
if nx < 2 or nz < 2 or num == 0:
return []
minx = float(x[0])
dx = float(x[1] - x[0])
u_arr = np.atleast_1d(np.asarray(u, dtype=float))
if u_arr.size == 1:
u_by_row = np.full(nz, float(u_arr[0]))
elif u_arr.size == nz:
u_by_row = u_arr
else:
# Caller gave an array of the wrong length — fall back to the mean so
# the plot still renders rather than raising mid-draw.
u_by_row = np.full(nz, float(np.mean(u_arr)))
dh = nz / num
lines = []
for j in range(num):
ycell = 1.0 + dh * j
if ycell < 1.0:
ycell = 1.0
if ycell > nz:
ycell = nz
yci = int(round(ycell) - 1)
yci = max(0, min(nz - 1, yci))
u_local = float(u_by_row[yci])
# 0.1 m/s floor prevents 1/u blowups at stagnant layers.
u_local = u_local if abs(u_local) > 0.1 else math.copysign(0.1, u_local) if u_local != 0 else 0.1
tstep = dx / u_local
xs = np.empty(nx)
ys = np.empty(nx)
xs[0] = minx
ys[0] = z[yci]
for i in range(1, nx):
xs[i] = x[i]
ys[i] = ys[i - 1] + tstep * w[yci, i]
lines.append((xs, ys))
return lines
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