Riemann invariants — where it appears
Named by 4 essays across 2 fields — each of them below, with the objects they name alongside it.
One diaphragm, every wave
Two states of the same gas at rest, separated by nothing, is the simplest initial condition compressible flow admits — and its answer contains all three waves the equations possess at once: a shock one way, an expansion fan the other, and between them a surface across which the density jumps and the pressure does not.
The wall that cancels its own waves
The area ratio of a supersonic nozzle fixes its exit Mach number and says nothing whatever about its shape. What fixes the shape is a wave-by-wave construction in which the wall turns through exactly the angle needed to absorb each expansion as it arrives — and getting it wrong leaves a stream full of oblique shocks at precisely the right Mach number.
Two numbers that do not change
One-dimensional unsteady gas flow carries two quantities that are exactly constant along two families of curves. That single fact turns a pair of coupled partial differential equations into a family of straight lines, and gives an exact speed at which a gas outruns its own expansion.
Twice the margin, on top of the hammer
Shut a valve on a line whose pressure is low and the returning wave boils the water beside it. When that cavity closes, the head at the valve can pass the Joukowsky rise — by up to twice the margin that let the water boil, in a sawtooth that jumps each time one more round trip fits into the cavity's life, and for a time that is shortest exactly when the pulse is tallest.
Named alongside it
The objects these essays reach for when they reach for this one.
Expansion fanCharacteristicsExact solutionIsentropicMethod of characteristicsModel limitArea machCavitationColumn separationConservationContact surfaceDiscontinuity