Skip to the simulation
Domi Jin / Thoughts and experimentsSources and scope ↗

GRAVITATIONAL-WAVE INSTRUMENTATION · AN INTERACTIVE SIMULATION

Atmospheric Newtonian noiseWhen the air above an observatory pulls directly on its mirrors.

No acoustic barrier can block gravity. Explore how passing infrasound wave packets and turbulent daytime air parcels couple gravitationally to suspended interferometer mirrors—and why thermal eddies force third-generation detectors deep underground.

Synced 3D physical scene + geometric modelLive 1D Kolmogorov Monte Carlo FFTaLIGO · ET · CE · TOBA · SOGRO

Based on Wenhui Wang's UT Arlington Ph.D. dissertation (2025) and the companion paper by Wenhui Wang & Teviet Creighton (2025). The direct MavMatrix PDF download returned HTTP 403 to automated retrieval, so all equations, environmental baselines, detector curves and 1D numerical validation steps implemented here come directly from Wang's dissertation record and the published companion paper (arXiv:2505.05690).

00

DUAL-STAGE ATMOSPHERIC FIELD SIMULATION · SYNCED MODEL

What moves around the test mass, and how the geometry maps to strain

Every temperature fluctuation or pressure wave in the open air pulls gravitationally on a detector's suspended mirrors through Newton's inverse-square law. Below, the rendered 3D scene (bedrock or shelter, vacuum tube, laser arm, moving air parcels) is paired side-by-side with the synced geometric model and camera frustum from Wang & Creighton (2025).

Drag rendered view on left → camera frustum & standoff geometry update live on right
Rendered 3D · Turbulent air parcelsCool dense parcelWarm buoyant eddy
Drag to orbit viewpoint · D_eff = 10.0 m · √S_h ≈ 9.7e-21 Hz⁻¹/²
Abstracted geometric model · syncedCycloid eddy (R = 1.20 m)f_eddy = 1.33 Hz · √S_h = 4.4e-19
Drag to orbit diagram · white frustum = rendered viewpoint

Why geometry bridges to strain: each cold/warm parcel pulls along δg_x ∝ x / r³. Smooth wind only fluctuates on the crossing timescale D / v (exponentially damped above it); cycloidal circulation of radius R modulates acceleration at f = v / (2πR), turning exponential shielding into a power-law tail.

TIDAL ACCELERATION PULSE δg_x(t) ALONG ARM AXISD_eff = 10.0 m
Smooth pass-by dipole ~ x / (x² + D²)³/²Cycloid eddy modulation injects power at Ω = v/Rparcel position relative to test mass (t = 0 overhead)
Infrasound (Q=1.5): 4.99e-22 Hz⁻¹/²Thermal (turbulent): 9.74e-21 Hz⁻¹/²3D active array (N): 6.7e+3 sensors
01

COHERENT VS INCOHERENT ACOUSTIC FIELDS · EQS. (5) & (10)

Infrasonic Newtonian noise and underground wave-packet floors

A perfectly coherent horizontal sound wave at speed v_s = 340 m/s is exponentially suppressed underground as e^(−ωD/v_s). Real atmospheric wave trains, however, stay spatially coherent only over a finite packet length l = Qλ, replacing pure exponential decay below e^(−πQ) with a weaker power-law tail.

95th-percentile noon infrasound (√S_P = 0.1 Pa/√Hz · f⁻¹)D = 100 m · L = 10 km
10^-2510^-2310^-2110^-1910^-1710^-150.1 Hz1 Hz10 Hz50 Hz
Coherent Q → ∞ (e^(−ωD/v_s))Wave packet Q = 1.0Dashed: shallow D = 3 m reference

Explore acoustic shielding

√S_h ∝ ω⁻² (1 + ωL/2v_s)⁻¹ (e^(−ωD/v_s) + e^(−πQ))
2 Hz coherent ASD1.08e-22
2 Hz packet ASD (Q=1.0)8.72e-23

Notice how small Q weakens surface pressure coherence below e^(−πQ) yet raises noise deep underground whenever D/λ > Q/2, because wave packets fail to cancel smoothly over the long crossing window D/v_s.

02

ADVECTED KOLMOGOROV TURBULENCE & 1D MONTE CARLO

Why turbulent wind turns an exponential cliff into a power law

Smooth uniform wind glides past a mirror over timescale D/v, dying off exponentially above f ~ v/(2πD). Once surface roughness or eddies roll air parcels along cycloidal loops of radius R = v/Ω, frozen temperature pockets re-accelerate near f = v/(2πR), lifting a steep f^(−29/6) locus into the gravitational-wave band.

Daytime peak thermal turbulence (c_T² = 0.2 K² m⁻²/³, L = 10 km)D = 10 m · v = 10 m/s
10^-2510^-2310^-2110^-1910^-1710^-150.1 Hz0.5 Hz1 Hz5 Hz10 Hz30 Hz
Dashed cyan: smooth e^(−ωD/v)Blue: broadband floor (Q=0.1)Amber: narrow-band locus (Q→∞)

Appendix A.1 · Live 1D Kolmogorov Monte Carlo

Generates a 1,024 m Gaussian parcel ribbon filtered in Fourier space to D_T(Δr) = 0.2 (Δr)^(2/3) K², orbits parcels on a cycloid of radius R at height D, sums G δm_i x_i/r_i³, and FFTs δg_x(t) in real time.


LIVE FFT SPECTRUM VS ANALYTIC 1D LOCUS EQ. (A.2)10^-2510^-2310^-2110^-1910^-170.2 Hz0.5 Hz1 Hz2 Hz5 Hz10 Hz

Predicted peak f = v/(2πR) = 1.99 Hz · Simulated normalized peak at 2.50 Hz (2.34e-21 vs Eq. A.2 1.98e-21 Hz⁻¹/², L = 4 km, θ = 40°, δA = 1 m²).

STRUCTURE FUNCTION VERIFICATION · D_T(Δr) = 0.2 Δr^(2/3)

Before computing gravitational pull, the generated 1D airmass is checked across lag scales Δr to verify the inertial-range Kolmogorov power law holds without artificial fine-tuning of spectral amplitude:

Δr = 0.25 m0.057 / 0.079 K²
Δr = 0.50 m0.115 / 0.126 K²
Δr = 1.00 m0.200 / 0.200 K²
Δr = 2.00 m0.335 / 0.317 K²
Δr = 4.00 m0.499 / 0.504 K²

Agreement in the inertial range (Δr ≥ 0.5 m) confirms both the spatial correlation slope and absolute temperature variance match Eq. (A.2) assumptions.

03

SECTION 4 BENCHMARKS · ALIGO, EINSTEIN TELESCOPE, COSMIC EXPLORER, GRADIOMETERS

Where atmospheric Newtonian noise bites into 2G, 3G and torsion detectors

Select an observatory from Section 4 of Wang & Creighton (2025) to overlay its digitized design sensitivity against the canonical 95th-percentile infrasound and daytime peak thermal bands at any siting depth D.

Einstein Telescope (ET)D = 100 m · v = 10 m/s
10^-2710^-2510^-2310^-2110^-1910^-1710^-150.11101001000
Cyan: ET design curveIndigo: Infrasound (Q=1 to Q→∞)Amber: Thermal (Q=0.1 to worst locus)

Siting depth & band budget

Thermal worst-locus exceedance1.6–6.8 Hz
Infrasound (Q=1) exceedanceBelow target

L = 10 km underground third-generation detector targeting ~2-10 Hz sensitivity (Punturo / ET sensitivities).

04

SURFACE ENCLOSURES D_EFF & VOLUMETRIC TOMOGRAPHY · §§2.3 & 5

Building a bigger hall versus mapping every cubic metre of wind

HEURISTIC SURFACE SHELTER STANDOFF D_EFF = ¼⟨r⁻¹⟩⁻¹

Because surface structures surround the test mass on three sides rather than only from above, the inverse-distance solid-angle integral compresses effective depth:

Paper ratio D_eff6.58 m
Uniform upper-hemisphere quadrature7.22 m

For a hemisphere of radius R = 6 m, D_eff = 3.0 m matches the roll-off of Fiorucci et al. (2018). For a half-cube, Wang & Creighton quote 0.5480 h whereas uniform upper-hemisphere numerical quadrature evaluates to 0.6015 h; either way, achieving D_eff = 100 m via an above-ground hangar would require a ~180 m structure, making underground siting far more practical (while simultaneously cutting seismic NN).

WHY ACTIVE THERMAL SUBTRACTION IS HARD · N ~ (2πf D / v)³

Coherent seismic and acoustic fields can be predicted from a sparse perimeter array. Incoherent thermal eddies have correlation length l_corr ~ v / ω and demand real-time 3D tomography throughout a hemisphere of radius D:

Independent 3D volumetric parcels per snapshot2.48e+5

Eddy correlation scale l = v/(2πf) = 1.59 m at v = 10 m/s. Achieving 100 m underground performance on the surface at 1 Hz requires ~10⁵–10⁶ independent sub-second temperature measurements to millikelvin precision—likely achievable only via remote atmospheric lidar or absorption-line tomography, placing solar-orbit missions in view for <1 Hz bands.

→

WHAT THIS CHANGES FOR OBSERVATORIES

Why thermal advection sets the low-frequency frontier

Coherent seismic and acoustic fluctuations can in principle be monitored with sparse seismometers or infrasound arrays and subtracted in feed-forward pipelines. Wind-advected temperature perturbations, however, carry correlation scales of only a couple of metres at 1 Hz—meaning atmospheric Newtonian noise acts as an irreducible siting constraint unless detectors bury test masses at least ~100 m underground (for 2–10 Hz sensitivity) or leave Earth's atmosphere behind in solar orbit below 1 Hz.