# Unsteady Laminar Stokes Layers > Use when you must compute the exact unsteady laminar Stokes layer of an infinite plate in a quiescent fluid, either impulsively started or oscillating in its own plane: for the stokes-first-problem Rayleigh layer of a plate started at speed U, evaluate the similarity profile u/U = erfc(y/(2*sqrt(nu*t))), the layer edge at 3.64*sqrt(nu*t) where u/U = 0.01, the wall shear decaying as 1/sqrt(t) from rho*U*sqrt(nu/(pi*t)), and the displacement thickness; for the stokes-second-problem oscillating-plate-layer at omega, evaluate the exponential-cosine velocity field, the penetration depth sqrt(2*nu/omega) with exp(-1) amplitude and 1-rad lag, and the wall shear amplitude rho*U*sqrt(nu*omega) leading the plate velocity by 45 degrees. Produces the closed-form velocity profiles, thicknesses and wall-shear histories in SI units for unsteady shear-layer and viscous time-scale checks. Trigger: unsteady-laminar-stokes-layers, stokes-first-problem, oscillating-plate-layer, rayleigh-layer. - Skill: `ashfordeou/unsteady-laminar-stokes-layers` (Agent Skill, multi-file: 3 files) - Install (CLI): `npx skillmds@latest add ashfordeou/unsteady-laminar-stokes-layers` - Raw SKILL.md: https://api.skillmd.com/api/skills/ashfordeou/unsteady-laminar-stokes-layers/raw - Safety review: pending - Works with: Claude Code, Claude.ai, OpenAI Codex - Category: Coding & Dev Tools - License: Apache-2.0 - Author: ashfordeOU (https://skillmd.com/u/ashfordeou) - Updated: 2026-09-17 - Page: https://skillmd.com/skills/ashfordeou/unsteady-laminar-stokes-layers --- # Unsteady Laminar Stokes Layers (aerodynamics/boundary-layer/unsteady-laminar-stokes-layers) Use when you must compute the exact unsteady laminar Stokes layer of an infinite flat plate in a quiescent half-space: the closed-form solutions of the one-dimensional vorticity diffusion equation u_t = nu * u_yy for a plate impulsively started at t = 0 (Stokes first problem, the Rayleigh layer) and for a plate oscillating in its own plane (Stokes second problem). The time-dependent layer is the unsteady member of the exact-viscous family whose steady members are already in the tree: the Blasius flat-plate boundary layer (boundary-layer-theory) and the shear-driven Couette gap (compressible-couette-flow). The aeroelasticity leaves cover only inviscid indicial airfoil response, so no existing leaf owns time-dependent laminar shear layers over a plate. Fully closed form, pure stdlib, no iteration. It does not do steady boundary layers, regime classification, Couette gap flow or inviscid oscillating-airfoil aerodynamics; incompressible constant-property laminar flow only, with uniform nu. ## Domain quick reference - Diffusion balance: u_t = nu * u_yy over the half-space y >= 0 above a plate at y = 0 in fluid at rest. Module constants: NU_AIR = 1.46e-5 m2/s, RHO_AIR = 1.225 kg/m3, DELTA99_COEF = 3.6428 (2 * 1.8214, where erfc(1.8214) = 0.01). Dynamic viscosity is always derived mu = rho * nu, never an input. - Stokes first problem (impulsive start, Rayleigh layer): the plate starts at speed U at t = 0 and the layer diffuses outward self-similarly with u/U = erfc(eta), similarity variable eta = y / (2 * sqrt(nu * t)); u(0, t) = U exactly for all t > 0 (no slip) and the profile shape is identical at every time. - Layer edge: delta = 3.6428 * sqrt(nu * t), where u/U = erfc(1.8214) = 0.0099994, the 99-percent-deficit point; delta grows as sqrt(t), delta(t2)/delta(t1) = sqrt(t2/t1), without bound. - First-problem wall shear: du/dy|0 = -U / sqrt(pi * nu * t), so tau_w = mu * |du/dy|0 = rho * U * sqrt(nu / (pi * t)), decaying as 1/sqrt(t); tau_w * sqrt(t) = rho * U * sqrt(nu / pi) exactly constant. - Displacement thickness: delta* = integral_0^inf (1 - u/U) dy = 2 * sqrt(nu * t / pi) (the half-space erfc integral is 1/sqrt(pi)); the momentum balance rho * U * d(delta*)/dt = tau_w holds identically. - Stokes second problem (oscillating plate): the plate moves as U * cos(omega * t) and the steady-periodic solution is u = U * exp(-y/delta) * cos(omega * t - y/delta) with wavenumber k = sqrt(omega / (2 * nu)) = 1/delta, penetration depth delta = sqrt(2 * nu / omega), the real part of U * exp(i * omega * t - (1 + i) * k * y). At depth y the amplitude is U * exp(-y/delta) and the signal lags the wall by y/delta radians; at y = delta the amplitude is exp(-1) * U = 0.3679 * U and the lag is exactly 1 rad (57.30 deg). - Second-problem wall shear: du/dy|0 = k * U * (sin(omega * t) - cos(omega * t)), so with the resistance-on-plate convention tau_w = -mu * du/dy|0 (positive resisting +x plate motion) tau_w(t) = tau_amp * cos(omega * t + pi / 4) with tau_amp = rho * U * sqrt(nu * omega) = mu * U * sqrt(omega / nu); the shear leads the plate velocity by 45 degrees (one-eighth period, T/8 = pi / (2 * omega)) and passes through zero at omega * t = pi/4. - SI units throughout: m/s, m, Pa, rad/s, s. ## Workflow 1. Fix the flow state: uniform kinematic viscosity nu, density rho and plate speed U; decide between the stokes-first-problem impulsive start (Rayleigh layer) and the stokes-second-problem plate oscillation at frequency omega. Dynamic viscosity is always mu = rho * nu. 2. First problem, similarity profile traverse: evaluate the erfc Rayleigh-layer profile with stokes_first_velocity(U, nu, y, t) = U * erfc(y / (2 * sqrt(nu * t))) at the stations y and times t of interest; u(0, t) = U at the wall and u/U collapses onto one erfc curve in eta at every time. 3. First problem, layer-edge traverse: locate the edge of the Rayleigh layer with rayleigh_layer_thickness(nu, t) = 3.6428 * sqrt(nu * t), the 99-percent-deficit point where u/U = 0.01, and scale it across times with the sqrt(t) growth law. 4. First problem, shear-decay traverse: evaluate the wall shear history with stokes_first_wall_shear(rho, U, nu, t) = rho * U * sqrt(nu / (pi * t)); check the 1/sqrt(t) decay with the tau_w * sqrt(t) invariant. 5. First problem, displacement-thickness traverse: compute the displacement thickness with stokes_first_displacement_thickness(nu, t) = 2 * sqrt(nu * t / pi) and confirm the momentum balance of the growing layer, rho * U * d(delta*)/dt = tau_w, by finite difference. 6. Second problem, penetration-depth traverse: evaluate the Stokes layer thickness with stokes_penetration_depth(nu, omega) = sqrt(2 * nu / omega), the depth of the exp(-1) amplitude point. 7. Second problem, oscillating-field traverse: evaluate the exponential-cosine velocity field with stokes_second_velocity(U, nu, omega, y, t) at the depths and phases of interest; the local amplitude is U * exp(-y/delta) and the phase lag is y/delta radians, so the field peaks at each depth one radian of omega * t after the wall does. 8. Second problem, shear-phase traverse: compute the wall shear amplitude with stokes_second_shear_amplitude(rho, U, nu, omega) = rho * U * sqrt(nu * omega) and its time history with stokes_second_wall_shear(rho, U, nu, omega, t) = tau_amp * cos(omega * t + pi / 4); the shear leads the plate velocity by 45 degrees and crosses zero at omega * t = pi/4, exactly T/8 after the wall velocity peak. 9. Input-rejection and determinism traverse: confirm every non-physical input (nu <= 0, t <= 0, y < 0, rho <= 0, omega <= 0) raises ValueError, then run the contract test scripts/test_unsteady_laminar_stokes_layers.py. ## Worked example Air at standard conditions, nu = 1.46e-5 m2/s, rho = 1.225 kg/m3, plate speed U = 30 m/s (real outputs of the module functions). Stokes first problem, plate started at t = 0: - Similarity profile u/U = erfc(eta) at t = 0.001 s (eta = 1 at y = 0.2417 mm): u/U = 0.723674 at eta = 0.25, 0.479500 at eta = 0.5, 0.157299 at eta = 1.0, 0.033895 at eta = 1.5, 0.0099994 at eta = 1.8214, 0.004678 at eta = 2.0; monotone from 1.000000 at the wall toward 0 in the far field. - Layer edge delta = 3.6428 * sqrt(nu * t): 0.4402 mm at t = 0.001 s, 1.392 mm at 0.01 s, 4.402 mm at 0.1 s, 13.92 mm at 1 s, 44.02 mm at 10 s, one hundred times thicker after four decades of time, with u/U = 0.0099994 at the edge at every time (self-similar collapse). - Wall shear decay tau_w = rho * U * sqrt(nu / (pi * t)): 2.505295 Pa at 0.001 s, 0.792244 Pa at 0.01 s, 0.250529 Pa at 0.1 s, 0.079224 Pa at 1 s, 0.025053 Pa at 10 s; tau_w(10 s) / tau_w(0.001 s) = 0.01 and tau_w * sqrt(t) = 0.0792244 Pa sqrt(s) constant. - Front arrival at y = 1 mm: 0.000000 m/s after 1 ms, 1.926887 m/s after 10 ms, 16.752282 m/s after 100 ms, 25.595499 m/s after 1 s. - Displacement thickness delta* = 2 * sqrt(nu * t / pi): 0.136343 mm at 1 ms, 13.6343 mm at 10 s; delta*/delta = 0.3098 always. - Momentum balance: rho * U * d(delta*)/dt over t = 1.0 to 1.02 s reproduces tau_w(1.01 s) with relative error 1.2e-5. Stokes second problem, plate oscillating at omega = 50 rad/s (period T = 0.12566 s): - Penetration depth delta = sqrt(2 * nu / omega) = 7.6419893e-4 m (0.7642 mm). - Amplitude profile U * exp(-y/delta) with phase lag y/delta: y/delta = 0: 30.0000 m/s, 0.00 deg; 0.5: 18.1959 m/s, 28.65 deg; 1.0: 11.0364 m/s, 57.30 deg (exp(-1) * U, lag exactly 1 rad); 2.0: 4.0601 m/s, 114.59 deg; 3.0: 1.4936 m/s, 171.89 deg. - Velocity at y = delta over a cycle: 5.9630 m/s at t = 0, 9.6853 m/s at t = 0.01 s, 11.0364 m/s at t = 0.02 s (the peak, one radian after the wall peak), 9.6853 m/s at t = 0.03 s, 0.7807 m/s at t = 0.05 s. - Wall shear amplitude tau_amp = rho * U * sqrt(nu * omega) = 0.992930 Pa, identical to mu * U * sqrt(omega / nu) (relative difference below 1e-12). Time history tau_w = tau_amp * cos(omega * t + pi / 4): 0.702108 Pa (0.707107 of the amplitude, cos 45 deg) at t = 0, 0.000000 Pa at t = 0.015708 s (omega * t = 45 deg), -0.992930 Pa at t = 0.047124 s (135 deg), -0.702108 Pa at t = 0.062832 s (180 deg). - Phase read-off: T/8 = 0.015708 s = pi / (4 * omega), and the shear zero crossing sits exactly one-eighth period after the wall velocity peak at t = 0: the shear waveform leads the plate velocity by 45 degrees. Read-off: a plate start in air at 30 m/s carries 2.5 Pa of wall shear for the first millisecond but only 0.025 Pa after 10 s while the affected layer grows from 0.44 mm to 44 mm; a 50 rad/s (about 8 Hz) oscillation at the same speed confines the motion to a 0.76 mm Stokes layer with shear swinging between plus and minus 0.99 Pa, peaking one-eighth period before the plate reaches peak speed. ## Verification - Confirm stokes_first_velocity(30.0, 1.46e-5, 0.0, 0.001) returns 30.0 exactly (erfc(0) = 1) and u/U at eta = 1 (y = 2 * sqrt(nu * t)) is 0.1572992071 within 1e-6. - Confirm rayleigh_layer_thickness(1.46e-5, 0.001) returns 4.40161e-4 m within 1e-6, u/U = 0.01 within 1e-3 at the edge, and delta(10 s) / delta(0.001 s) = 100 = sqrt(10 / 0.001). - Confirm stokes_first_wall_shear(1.225, 30.0, 1.46e-5, 0.001) returns 2.505295 Pa within 1e-3 (between 2.0 and 3.0 Pa), the decay ratio tau_w(10 s) / tau_w(0.001 s) is 0.01, and tau_w * sqrt(t) = 0.0792244 Pa sqrt(s) is constant. - Confirm the momentum balance: rho * U * (delta*(1.02) - delta*(1.0)) / 0.02 reproduces tau_w(1.01 s) within 1e-3 relative (anchor error 1.2e-5), and delta*/delta = 0.3098 within 1e-3. - Confirm stokes_penetration_depth(1.46e-5, 50.0) returns 7.64199e-4 m within 1e-8, u(0, t) = U * cos(omega * t), the signal at y = delta peaks at t = 1/omega at exp(-1) * U = 11.0364 m/s, and the amplitude at y = 3 * delta is 1.4936 m/s. - Confirm stokes_second_shear_amplitude(1.225, 30.0, 1.46e-5, 50.0) returns 0.992930 Pa within 1e-4 (between 0.9 and 1.1 Pa) and equals mu * U * sqrt(omega / nu) within 1e-12 relative; tau_w(0) / tau_amp = cos(pi / 4) = 0.707107, tau_w vanishes at t = pi / (4 * omega) (residual 6.08e-17 Pa), and tau_w = -tau_amp at t = 3 * pi / (4 * omega). - Confirm every non-positive nu, rho, omega and t and every negative y raises ValueError, and that repeated calls are bit-identical (deterministic, stdlib math only). - Run the contract test offline: python3 scripts/test_unsteady_laminar_stokes_layers.py (32 tests, deterministic). ## Related leaves - aerodynamics/boundary-layer/boundary-layer-theory: the steady Blasius flat-plate member of the exact-viscous family; the Rayleigh layer is its unsteady counterpart driven by the plate momentum rather than the free stream. - aerodynamics/boundary-layer/boundary-layer-transition, aerodynamics/boundary-layer/boundary-layer-separation, aerodynamics/boundary-layer/stagnation-flow-boundary-layer, aerodynamics/boundary-layer/rough-wall-skin-friction: the rest of the boundary-layer pack, all steady-state content. - aerodynamics/high-speed/compressible-couette-flow: the steady shear-driven gap between two plates with a linear velocity profile, the other exact solution of the viscous diffusion balance; this leaf covers the unsteady half-space layer driven by one moving surface. - aerodynamics/aeroelasticity/aeroelastic-gust-response and aerodynamics/aeroelasticity/flutter-speed-prediction: the inviscid unsteady-airfoil leaves (indicial response and oscillating-airfoil loads), which share time-dependence but no viscous-layer physics. - aerodynamics/high-speed/shock-tube: the compressible unsteady expansion wave, a wave process rather than a viscous Stokes layer. ## Pitfalls - Expecting the layer to reach a steady state: the Rayleigh layer of the impulsively started plate keeps growing as sqrt(nu * t) forever (0.44 mm after 1 ms, 44 mm after 10 s), and its wall shear keeps decaying as 1/sqrt(t); there is no equilibrium thickness in the first problem. - Confusing the two layer edges: the first-problem 99-percent edge is 3.6428 * sqrt(nu * t) and grows in time, while the second-problem penetration depth sqrt(2 * nu / omega) is fixed by the frequency; at the second-problem depth the amplitude is exp(-1) * U = 0.3679 * U, not 0.01 * U. - Reading the shear phase sign backwards: with the resistance convention tau_w = -mu * du/dy|0 (positive resisting +x plate motion) the oscillating-plate wall shear tau_amp * cos(omega * t + pi / 4) LEADS the plate velocity by 45 degrees and passes through zero at omega * t = pi/4, one-eighth period AFTER the plate reaches peak speed; a shear that lagged the wall motion would put the zero crossing elsewhere in the cycle. - Using a steady skin-friction correlation for an impulsive start: the first-problem wall shear rho * U * sqrt(nu / (pi * t)) is singular at t = 0 and decays as 1/sqrt(t); a steady correlation has no time argument and cannot represent the transient. - Treating the second problem as a start-up: stokes_second_velocity and stokes_second_wall_shear describe the steady-periodic state and accept any real t, including negative t; the initial transient after the oscillation is switched on is not part of this closed form. - Passing rho where nu belongs: dynamic viscosity is always derived mu = rho * nu; the shear functions take (rho, U, nu, ...) and the velocity functions take (U, nu, ...), so swapping rho into a velocity call silently mis-scales the profile. ## Behavior contract (gate 3) Run the deterministic contract test (stdlib unittest, offline): python3 scripts/test_unsteady_laminar_stokes_layers.py The 32-test contract covers the worked example of the impulsively started plate (erfc similarity profile against math.erfc, eta = 1 anchor, far-field decay, front arrival at a fixed station), the Rayleigh layer edge (anchor thickness, u/U = 0.01 at the edge, sqrt(t) growth ratio), the wall shear decay (anchor value and magnitude bound, decade ratio 0.01, tau_w * sqrt(t) invariant), the displacement thickness and its 0.3098 ratio with the momentum balance identity, the oscillating-plate layer (penetration depth anchor, no-slip cosine, phase-zero local amplitude, cycle samples at y = delta, amplitude profile decay), the wall shear amplitude and phase (anchor value and magnitude bound, mu identity, 45 degree phase lead, zero crossing at omega * t = pi/4, negative peak, one-eighth-period read-off), and ValueError rejection of every non-physical input class with the determinism and stdlib-only checks. It passes under both /usr/bin/python3 and the pyenv 3.13.12 hook interpreter. ## Compliance - Standards referenced, not reproduced: NACA-TR-824 is the sibling precedent for the viscous-layer family (standards-map.yaml); the classical treatment of unsteady laminar boundary layers follows Schlichting, whose material is cited through the report. The relations above are standard engineering methodology, summary-only. - compliance: STANDARDS-REF, gated: false.