The organising axis

Every figure, by regime

A shape does not decide how a fluid behaves around it. One dimensionless number does, and the same cylinder creeps, sheds or goes turbulent as that number crosses its thresholds. This is every figure on the site sorted by the hypothesis it was drawn under.

Every figure here carries a strip along its foot naming two things: the model that produced it, and the regime it holds in. That is an invariant of this site rather than a courtesy — a result quoted without its Reynolds or Mach number is a result quoted without its hypothesis, and a figure that cannot state its regime throws and stops the build.

This page is built by rendering all 3946 figure placements and reading those strips back out of the finished SVG, rather than from the code that wrote them. The two can differ, and where they do it is the picture that is right. 164 of the 171 generators used in essays are called at more than one regime, which is the difference between a family of figures and one picture shown repeatedly.

The bands below are one page each. They were one page in total until the collection passed three hundred and seventy essays, at which point the combined listing went past the raw-byte budget this site holds every page to — so the index carries the counts and each hypothesis carries its own rows.

Kinematics only — an identity about the field, whatever moves it

37 figures

Any Reynolds number — viscosity is absent

1209 figures

An exact Beltrami solution of Euler — steady, inviscid, three-dimensional

10 figures

Re → 0 — creeping flow, inertia absent

157 figures

Set by the reduced Reynolds number Re·(h/L) — not by Re

2 figures

Set by the film's aspect ratio — one length small enough to delete inertia

35 figures

Re below 1 — creeping, no wake at all

13 figures

Re 1 to 47 — attached, or a steady standing pair

22 figures

Re 47 to 10³ — the wake sheds

35 figures

Re 10³ to 2·10⁵ — laminar separation, wide wake

22 figures

Re above 2·10⁵ — turbulent boundary layer

19 figures

Swept in Reynolds number — the figure is about the variation, not one value

41 figures

Swept in pipe Reynolds number — the figure is about the variation

14 figures

Re below 2300 in a pipe — the exact solution, and the flow takes it

13 figures

Set by the channel Reynolds number — internal flow between walls

24 figures

Set by the pipe Reynolds number — internal flow, not a wake

93 figures

Set by the wedge angle and the flux — a purely radial similarity flow

15 figures

Set by the suction coefficient — a layer held at a fixed thickness

7 figures

Set by the vortex Reynolds number Γ/ν — circulation against viscosity

17 figures

Swept in pore Reynolds number — the figure is about where the linear law stops

7 figures

Set by the jet's own Reynolds number — its width and its centreline speed

8 figures

Re_p below 10 in a bed — Darcy's law, and the linear term carries it

3 figures

Re_p 10 to 86 in a bed — both of Ergun's terms matter

3 figures

Set by the pore Reynolds number — a bed, not a body in a stream

16 figures

Set by the Womersley number — the radius against a cycle's diffusion depth

33 figures

Set by the position along a duct — x⁺ = x/(D·Re·Pr), axial conduction dropped

6 figures

An averaged wall condition — one length standing in for a structure

8 figures

Set by the Péclet number — advection against molecular diffusion

21 figures

Set by the tip-speed and advance ratios — a rotor with blades rather than a disc

28 figures

Boundary-layer theory — Re large enough that the layer is thin, and the number cancels

69 figures

Set by the reduced frequency — linear unsteady aerofoil theory, planar wake

28 figures

Set by the reduced frequency — how much of its own wake the section is still in

25 figures

Trimmed level flight — the hypothesis is a force and a moment balance

9 figures

Set by the Keulegan–Carpenter number — whether the flow has time to make a wake

20 figures

Set by a stated gust distribution — the average of a curve, not of a flow

7 figures

A self-excited oscillator — a caricature of a wake, with no fluid in it

13 figures

The limit of vanishing viscosity — where the answer does not follow the parameter

4 figures

Second order in the amplitude — a mean flow driven by an oscillation with none

17 figures

Set by being local — an exponent the geometry fixes, at any scale

10 figures

A truncation — a model system standing in for a flow, and named as one

37 figures

Stated in the wall's own variables — a friction velocity, a roughness, a kappa

33 figures

Set by a stated closure — a model rather than the equations

82 figures

Set by the class of fields compared — same boundary values, same flux

14 figures

Set by the Rayleigh number — buoyancy against diffusion

28 figures

Set by the Brinkman number — the heat a shear makes against the heat conducted away

7 figures

Vorticity as an object — a sheet, a patch or a filament, inviscid throughout

36 figures

The narrow-gap limit — a Taylor number that is also a Rayleigh number

12 figures

A topological count — linking and writhe, of curves rather than of a field

7 figures

Set by the domain's symmetry — images where they exist, a map where they do not

8 figures

Linear free-surface theory — an inviscid flow that radiates, and therefore drags

9 figures

An ensemble statistic — a distribution over material elements, not a field

8 figures

Set by the cavitation number — the pressure margin above vapour

65 figures

Set by the fluid's transport coefficients — a stated gas at a stated state

4 figures

Stated by the turbulence's own statistics — a dissipation, a scale, a spectrum

91 figures

Set by the Ekman number — viscosity against the planet's rotation

27 figures

A closure evaluated in a strain — a model's own algebra, with no flow round it

3 figures

A reduced set of equations — Prandtl's, Stokes' or the triple deck's, with what was dropped named

21 figures

Set by the Rossby number — inertia against the planet's rotation

25 figures

A comparison class at fixed boundary data — admissible fields, with no equation being solved

7 figures

A translating body's dipole — added mass from the disturbance's own energy, inviscid

5 figures

Set by the pressure's own Poisson equation — its source is Q, and the sign of Q decides

5 figures

A resultant on a closed contour — the shape entering only through the circulation

5 figures

A loading in harmonics — where the induced drag is a sum of squares of the departure

7 figures

An aeroelastic boundary — a root of the characteristic quartic, quasi-steady

4 figures

A yield stress — a fluid with a threshold below which it does not shear at all

8 figures

A converging film — Reynolds' equation, whose load separates into a bracket in the taper alone

6 figures

A free jet's similarity solution — momentum conserved, the scale fitted

7 figures

A field built from a stated spectrum — a statistic, not a solution

35 figures

Linear stability of a parallel flow — an eigenvalue problem with no Reynolds number in it

6 figures

A constructed solenoidal field — exact derivatives, and not a solution of anything

4 figures

A chaotic advection map — deterministic, area-preserving, and exponentially unpredictable

32 figures

A shock read by its strength — the expansion of the Hugoniot about a sound wave

1 figure

Set by the intermittency factor — turbulent some of the time

17 figures

The method of characteristics — one-dimensional unsteady flow, with two invariants

26 figures

A wave's second-order transport — a constraint on an integral, and not on a profile

4 figures

A logarithmic correction — exact in a limit, and approached at a constant rate per decade

9 figures

A shell model — a nonlinear cascade with no space in it

14 figures

A number's provenance — how it was located, rather than what flow it belongs to

2 figures

Fully developed duct flow — the Reynolds number scaled out, leaving only the cross-section

8 figures

Set by the boundary data and the mesh — an elliptic solve, not a flow model

7 figures

Set by a ratio of two lengths — a slenderness expansion, and no flow in the group

6 figures

Set by an imported flux law — a scalar conservation law, and no momentum equation

18 figures

Incompressible — Ma → 0, and nothing else assumed

204 figures

Ma below 0.3 — density effectively fixed

19 figures

Ma 0.3 to 0.8 — compressible, still subsonic

10 figures

Ma near 1 — transonic

12 figures

Ma above 1.2 — supersonic

77 figures

Set by the Mach number

117 figures

Set by the source's compactness and Mach number — linear acoustics

42 figures

Swept in Mach number — the figure is about the variation, not one value

98 figures

One-dimensional duct flow — the Mach number is the coordinate, not the setting

53 figures

Set by the θ–β–M relation — oblique shocks, and a deflection budget

8 figures

A curved shock whose shape is a model and whose jumps are exact

8 figures

Set by the heat release — one step, in equilibrium, and no chemistry in it

12 figures

The transonic small-disturbance equation — the perturbation decides the type

2 figures

The strong-shock limit — the ambient pressure is negligible

23 figures

The thin shock layer — γ and the density ratio decide it, and M∞ has dropped out

6 figures

Set by the caloric model — vibration in equilibrium, and no dissociation

18 figures

A lossless simple wave — finite amplitude, and no dissipation of any kind

7 figures

Whitham's weak-shock ageing — a far field reached by a signature, not by a body

8 figures

Slender-body theory — the drag is a functional of the area distribution alone

6 figures

Set by the Froude number — gravity against inertia

65 figures

Set by the buoyancy frequency — stratification against shear or forcing

19 figures

Set by the Grashof number — buoyancy with no imposed speed anywhere

9 figures

Set by the Bond or Weber number — surface tension against weight or inertia

55 figures

Set by the Deborah number — a relaxation time against an observation time

17 figures

Set by the viscosity and the Prandtl number inside the shock — continuum, at its edge

6 figures

Set by the Knudsen number — where the continuum stops

7 figures

Not a solved field — an axis, a count or a comparison

73 figures

The singular limit — a model problem standing in for a vanishing viscosity

5 figures

A singular perturbation — the hypothesis is the small parameter, not a fluid

7 figures

Prior to any regime — true before a flow is chosen

50 figures

Arithmetic — true of any field, and of no fluid in particular

23 figures

The generators, by how far they are stretched

How many distinct regimes each generator has been asked to draw. One is a picture; several is a family.

The figure library · What is refuted here · All essays