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from __future__ import annotations
import ast
import csv
import math
import re
import subprocess
from pathlib import Path
ROOT = Path("/home/user/Desktop")
CASE = ROOT / "airfoil"
COEFFICIENTS = CASE / "postProcessing/forces/0/forceCoeffs.dat"
def read(path: Path) -> str:
return path.read_text(encoding="utf-8", errors="ignore")
def named_block(text: str, name: str) -> str:
text = re.sub(r"/\*.*?\*/|//[^\n]*", "", text, flags=re.S)
match = re.search(rf"(?m)^\s*{re.escape(name)}\s*\{{", text)
if not match:
raise ValueError(f"missing block {name}")
start = text.find("{", match.start())
depth = 0
for index in range(start, len(text)):
depth += text[index] == "{"
depth -= text[index] == "}"
if depth == 0:
return text[start + 1 : index]
raise ValueError(f"unterminated block {name}")
def paren_section(text: str, name: str) -> str:
match = re.search(rf"(?m)^\s*{re.escape(name)}\s*\(", text)
if not match:
raise ValueError(f"missing section {name}")
start = text.find("(", match.start())
depth = 0
for index in range(start, len(text)):
depth += text[index] == "("
depth -= text[index] == ")"
if depth == 0:
return text[start + 1 : index]
raise ValueError(f"unterminated section {name}")
def has_entry(block: str, key: str, value: str) -> bool:
return re.search(rf"(?<!\w){re.escape(key)}\s+{value}\s*;", block) is not None
def close(actual: float, expected: float, tolerance: float) -> bool:
return math.isfinite(actual) and abs(actual - expected) <= tolerance
def python_script_is_valid(path: Path, required_fragments: tuple[str, ...]) -> bool:
text = read(path)
try:
tree = ast.parse(text)
except SyntaxError:
return False
return bool(tree.body)
def log_finished(path: Path) -> bool:
text = read(path)
return "foam fatal" not in text.lower() and text.rstrip().endswith("End")
def patch(text: str, name: str) -> str:
return named_block(named_block(text, "boundaryField"), name)
def face_count(block: str) -> int:
match = re.search(r"\bfaces\s*\((.*?)\)\s*;", block, re.S)
return len(re.findall(r"\([^()]+\)", match.group(1))) if match else 0
def mesh_vertices(mesh: str) -> list[tuple[float, float, float]]:
number = r"[-+]?(?:\d+(?:\.\d*)?|\.\d+)(?:[eE][-+]?\d+)?"
return [
tuple(float(value) for value in match)
for match in re.findall(
rf"\(\s*({number})\s+({number})\s+({number})\s*\)",
paren_section(mesh, "vertices"),
)
]
def airfoil_geometry_is_valid(mesh: str) -> bool:
count = 161
vertices = mesh_vertices(mesh)
if len(vertices) != 4 * count:
return False
inner0 = vertices[:count]
outer0 = vertices[count : 2 * count]
inner1 = vertices[2 * count : 3 * count]
outer1 = vertices[3 * count :]
expected: list[tuple[float, float]] = []
for index in range(81):
x = 0.5 * (1.0 + math.cos(math.pi * index / 80.0))
y = 5.0 * 0.12 * (
0.2969 * math.sqrt(x)
- 0.1260 * x
- 0.3516 * x**2
+ 0.2843 * x**3
- 0.1015 * x**4
)
expected.append((x, y))
for index in range(79, -1, -1):
x = 0.5 * (1.0 + math.cos(math.pi * index / 80.0))
y = -5.0 * 0.12 * (
0.2969 * math.sqrt(x)
- 0.1260 * x
- 0.3516 * x**2
+ 0.2843 * x**3
- 0.1015 * x**4
)
expected.append((x, y))
for actual, target in zip(inner0, expected):
if abs(actual[0] - target[0]) > 2.0e-10 or abs(actual[1] - target[1]) > 2.0e-10 or abs(actual[2]) > 1.0e-12:
return False
for lower, upper in zip(inner0, inner1):
if abs(lower[0] - upper[0]) > 1.0e-12 or abs(lower[1] - upper[1]) > 1.0e-12 or abs(upper[2] - 0.01) > 1.0e-12:
return False
for index, (x, y, _) in enumerate(inner0):
lower_outer = outer0[index]
upper_outer = outer1[index]
if (
not all(math.isfinite(value) for value in lower_outer + upper_outer)
or abs(lower_outer[0] - upper_outer[0]) > 1.0e-10
or abs(lower_outer[1] - upper_outer[1]) > 1.0e-10
or abs(lower_outer[2]) > 1.0e-12
or abs(upper_outer[2] - 0.01) > 1.0e-12
):
return False
offset_x = lower_outer[0] - x
offset_y = lower_outer[1] - y
if abs(math.hypot(offset_x, offset_y) - 5.0) > 5.0e-6:
return False
if offset_x * (x - 0.5) + offset_y * y <= 0.0:
return False
return True
def internal_field(path: Path, kind: str) -> list:
text = read(path)
header = named_block(text, "FoamFile")
match = re.search(
rf"internalField\s+nonuniform\s+List<{kind}>\s+(\d+)\s*\((.*?)\)\s*;",
text,
re.S,
)
if not match:
raise ValueError(f"missing {kind} field")
if kind == "vector":
values = [
tuple(float(value) for value in item.split())
for item in re.findall(r"\(([^()]+)\)", match.group(2))
]
valid_values = all(
len(value) == 3 and all(math.isfinite(item) for item in value)
for value in values
)
elif kind == "scalar":
values = [float(value) for value in match.group(2).split()]
valid_values = all(math.isfinite(value) for value in values)
else:
raise ValueError(f"unsupported field kind {kind}")
if (
len(values) != int(match.group(1))
or not values
or not valid_values
or not has_entry(header, "format", r"ascii")
or not has_entry(header, "class", rf"vol{kind.capitalize()}Field")
or not has_entry(header, "object", re.escape(path.name))
):
raise ValueError(f"invalid {kind} field")
return values
def coefficient_history() -> list[tuple[float, float, float]]:
history = []
header = None
for line in read(COEFFICIENTS).splitlines():
stripped = line.strip()
if stripped.startswith("# Time"):
header = " ".join(stripped.split())
continue
if not stripped or stripped.startswith("#"):
continue
values = [float(value) for value in stripped.split()]
if len(values) >= 4:
history.append((values[0], values[2], values[3]))
if header != "# Time Cm Cd Cl Cl(f) Cl(r)":
raise ValueError("unexpected OpenFOAM 11 forceCoeffs header")
return history
def history_is_complete(history: list[tuple[float, float, float]]) -> bool:
if len(history) != 1001:
return False
return all(
close(iteration, float(index), 1.0e-9)
and math.isfinite(cd)
and math.isfinite(cl)
for index, (iteration, cd, cl) in enumerate(history)
)
def check_case() -> bool:
mesh = read(CASE / "system/blockMeshDict")
build_script = read(ROOT / "build_case.py")
velocity = read(CASE / "0/U")
pressure = read(CASE / "0/p")
kinetic = read(CASE / "0/k")
omega = read(CASE / "0/omega")
nut = read(CASE / "0/nut")
physical = read(CASE / "constant/physicalProperties")
momentum = read(CASE / "constant/momentumTransport")
control = read(CASE / "system/controlDict")
schemes = read(CASE / "system/fvSchemes")
solution = read(CASE / "system/fvSolution")
boundary = read(CASE / "constant/polyMesh/boundary")
mesh_boundary = mesh
forces = named_block(named_block(control, "functions"), "forces")
simple = named_block(solution, "SIMPLE")
return all(
(
airfoil_geometry_is_valid(mesh),
mesh.count("hex (") == 161,
len(re.findall(r"\(\s*80\s+1\s+1\s*\)\s*simpleGrading\s*\(\s*80\s+1\s+1\s*\)", mesh)) == 161,
has_entry(named_block(mesh_boundary, "FARFIELD"), "type", r"patch"),
has_entry(named_block(mesh_boundary, "WALL10"), "type", r"wall"),
has_entry(named_block(mesh_boundary, "SYMP3"), "type", r"empty"),
face_count(named_block(mesh_boundary, "FARFIELD")) == 161,
face_count(named_block(mesh_boundary, "WALL10")) == 161,
face_count(named_block(mesh_boundary, "SYMP3")) == 322,
any(
re.search(r"\binternalField\s+uniform\s+\(0\.9961946981\s+0\.08715574275\s+0(?:\.0+)?\)\s*;", text) is not None
for text in (velocity, build_script)
),
has_entry(patch(velocity, "FARFIELD"), "type", r"freestreamVelocity"),
has_entry(patch(velocity, "FARFIELD"), "freestreamValue", r"uniform\s+\(0\.9961946981\s+0\.08715574275\s+0(?:\.0+)?\)"),
has_entry(patch(velocity, "WALL10"), "type", r"noSlip"),
has_entry(patch(velocity, "SYMP3"), "type", r"empty"),
has_entry(patch(pressure, "FARFIELD"), "type", r"freestreamPressure"),
has_entry(patch(pressure, "FARFIELD"), "freestreamValue", r"uniform\s+0(?:\.0+)?"),
has_entry(patch(pressure, "WALL10"), "type", r"zeroGradient"),
has_entry(patch(kinetic, "FARFIELD"), "type", r"inletOutlet"),
has_entry(patch(kinetic, "FARFIELD"), "inletValue", r"uniform\s+0\.001"),
has_entry(patch(kinetic, "WALL10"), "type", r"kqRWallFunction"),
has_entry(patch(omega, "FARFIELD"), "type", r"inletOutlet"),
has_entry(patch(omega, "FARFIELD"), "inletValue", r"uniform\s+10(?:\.0+)?"),
has_entry(patch(omega, "WALL10"), "type", r"omegaWallFunction"),
has_entry(patch(nut, "WALL10"), "type", r"nutkWallFunction"),
all(has_entry(patch(field_text, "SYMP3"), "type", r"empty") for field_text in (pressure, kinetic, omega, nut)),
re.search(r"\bnu\s+\[0 2 -1 0 0 0 0\]\s+1e-?5\s*;", physical, re.I)
is not None,
has_entry(momentum, "model", r"kOmegaSST"),
re.search(r"\bendTime\s+1000\s*;", control) is not None,
re.search(r"\bwriteFormat\s+ascii\s*;", control) is not None,
has_entry(forces, "type", r"forceCoeffs"),
has_entry(forces, "writeInterval", r"1"),
has_entry(forces, "patches", r"\(\s*WALL10\s*\)"),
has_entry(forces, "rhoInf", r"1(?:\.0+)?"),
has_entry(forces, "magUInf", r"1(?:\.0+)?"),
has_entry(forces, "lRef", r"1(?:\.0+)?"),
has_entry(forces, "Aref", r"0\.01"),
has_entry(forces, "dragDir", r"\(0\.9961946981\s+0\.08715574275\s+0(?:\.0+)?\)"),
has_entry(forces, "liftDir", r"\(-0\.08715574275\s+0\.9961946981\s+0(?:\.0+)?\)"),
all(has_entry(named_block(schemes, "divSchemes"), key, r"bounded\s+Gauss\s+upwind") for key in ("div(phi,U)", "div(phi,k)", "div(phi,omega)")),
"corrected" in named_block(schemes, "laplacianSchemes"),
has_entry(named_block(named_block(solution, "solvers"), "p"), "solver", r"GAMG"),
has_entry(simple, "nNonOrthogonalCorrectors", r"1"),
re.search(r"\bSYMP3\b.*?type\s+empty;", boundary, re.S) is not None,
)
)
def check() -> bool:
required = (
ROOT / "build_case.py",
ROOT / "postprocess.py",
ROOT / "summary.txt",
ROOT / "force_coefficients.csv",
CASE / "log.blockMesh",
CASE / "log.checkMesh",
CASE / "log.potentialFoam",
CASE / "log.simpleFoam",
CASE / "1000/U",
CASE / "1000/p",
CASE / "1000/k",
CASE / "1000/omega",
COEFFICIENTS,
)
if any(not path.is_file() or path.stat().st_size == 0 for path in required):
return False
if not python_script_is_valid(
ROOT / "build_case.py",
("airfoil", "naca_thickness", "blockMeshDict", "forceCoeffs", "0/U", "0/p"),
):
return False
if not python_script_is_valid(
ROOT / "postprocess.py",
("forceCoeffs.dat", "force_coefficients.csv", "summary.txt", "avg_cd", "avg_cl"),
):
return False
solve_log = read(CASE / "log.simpleFoam")
if any(
not log_finished(path)
for path in (CASE / "log.blockMesh", CASE / "log.checkMesh", CASE / "log.potentialFoam")
):
return False
if not log_finished(CASE / "log.simpleFoam") or "Time = 1000" not in solve_log:
return False
mesh_check = subprocess.run(
[
"bash",
"--noprofile",
"--norc",
"-c",
"trap - CHLD; . /opt/openfoam11/etc/bashrc && checkMesh -case /home/user/Desktop/airfoil",
],
stdout=subprocess.PIPE,
stderr=subprocess.STDOUT,
text=True,
timeout=120,
)
if (
mesh_check.returncode != 0
or "Mesh OK." not in mesh_check.stdout
or "Failed " in mesh_check.stdout
or "foam fatal" in mesh_check.stdout.lower()
or not mesh_check.stdout.rstrip().endswith("End")
or not check_case()
):
return False
velocity = internal_field(CASE / "1000/U", "vector")
pressure = internal_field(CASE / "1000/p", "scalar")
turbulent_k = internal_field(CASE / "1000/k", "scalar")
omega = internal_field(CASE / "1000/omega", "scalar")
if not (len(velocity) == len(pressure) == len(turbulent_k) == len(omega) == 12880):
return False
history = coefficient_history()
if not history_is_complete(history):
return False
window = [row for row in history if 800.0 <= row[0] <= 1000.0]
avg_cd = sum(row[1] for row in window) / len(window)
avg_cl = sum(row[2] for row in window) / len(window)
std_cd = math.sqrt(sum((row[1] - avg_cd) ** 2 for row in window) / len(window))
std_cl = math.sqrt(sum((row[2] - avg_cl) ** 2 for row in window) / len(window))
if not (0.1 < avg_cl < 2.0 and 0.001 < avg_cd < 0.2 and std_cl < 0.02 and std_cd < 0.01):
return False
keys = ("iteration", "cd", "cl")
with (ROOT / "force_coefficients.csv").open(encoding="utf-8", newline="") as stream:
rows = list(csv.DictReader(stream))
if len(rows) != len(history) or set(rows[0]) != set(keys):
return False
for row, expected in zip(rows, history):
actual = tuple(float(row[key]) for key in keys)
if any(not close(a, b, 5.0e-7) for a, b in zip(actual, expected)):
return False
values = [item.strip() for item in read(ROOT / "summary.txt").strip().split(",")]
if len(values) != 2:
return False
reported = tuple(float(value) for value in values)
expected = (avg_cl, avg_cd)
return all(math.isfinite(value) for value in reported) and all(
abs(actual - target) <= 5.0e-7 for actual, target in zip(reported, expected)
)
def main() -> int:
try:
result = check()
except Exception:
result = False
print("True" if result else "False")
return 0
if __name__ == "__main__":
raise SystemExit(main())
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