Fluid Flow & Aerodynamics
why things fly, and why the usual explanation is wrong
Theme

The thread: What is conserved — page 39

Page 39 of 43, continuing through the 384 essays this motif runs through.

384 essays carry this thread — page 39 of 43.

The longer a pair remembers, the less its cloud has tails. The kurtosis of the pairs' separation, ⟨r⁴⟩/⟨r²⟩², against how long each pair keeps its relative velocity, in units of the turnover time of eddies of its own size. Richardson's memoryless diffusion gives 3.76, dashed, with long tails of pairs that separate fast by chance; a Gaussian cloud gives 5/3. A memory of a tenth of a turnover time already takes the kurtosis to 2.55; one turnover time, to 1.82. The cloud's shape is a measurement of the memory. Transition and turbulence

A pair's memory shapes the cloud it spreads into

Richardson's diffusion of pair separations has no memory: each moment's push is independent of the last, and the cloud of separations grows as t³ with a peaked shape and long tails. Real pairs keep their relative velocity for about the turnover time of eddies their own size. Give them that memory and the cube law survives, because it is dimensional, but everything else about the cloud changes: its constant falls, its tails shrink, and its shape becomes a measure of how long a pair remembers. A memory of a tenth of a turnover time already takes the kurtosis from 3.76 to 2.5.

 The suction a diffuser needs to beat Betz on its own exit. The best power per unit of exit area against the suction held behind the exit, as a pressure coefficient −c. The curve is (2/3√3)(1 + c)^(3/2) up to c = ½ and the dots are a direct search. It starts at 0.385, sixty-five per cent of Betz's limit, and crosses 16/27 at c = 1/3 exactly — the pressure on the back face of Betz's open disc. A diffuser with no suction at its exit is worse than a bare rotor as large as its exit; one that beats the limit on its exit area is holding more suction there than the open disc holds behind itself. Fluids at work

A duct beats Betz only on the area it chooses

Put a wind turbine inside a flaring duct and it can take more than 16/27 of the wind's power through its rotor, which is the claim. Measure the same power against the duct's exit, the area the device actually fills in the wind, and a plain diffuser takes less than a bare rotor of that size would. It crosses the limit only when the duct holds a suction behind its exit, and the suction it needs is exactly the pressure on the back face of Betz's own disc.

 A long line empties from the break backwards. The pressure along a gas line three hundred friction lengths long — fL/D = 300 — at five times after it breaks at its far end into still air at a twentieth of its pressure, the break on the right. Half a transit time in, the rarefaction has crossed half the line and the gas beyond it has not moved. Friction then holds the pressure in a slope that lengthens back towards the closed end; at six transit times the closed end is at 0.55 of its starting pressure, at fifteen 0.21, and the break has long since stopped being choked. Compressible flow

A broken line empties at the pace of its friction

When a gas line breaks, its open end chokes and the textbook stops there: a choked outlet passes gas at its own speed of sound and nothing downstream can change that. On a long line the choke is the least of it. The break stays choked only while friction lets enough gas reach it, which on a line a thousand friction lengths long is the first eighth of the time to half pressure. The pressure falls at a pace friction sets, the half-time grows as the square root of the line's length in friction lengths, and the wall's heat — negligible in the steady line — makes the blowdown a third slower.

 The fuselage's overspeed reaches along the wing. The extra axial speed the fuselage alone gives the air beside it, as a fraction of the flight speed, against distance out along the wing from the fuselage's axis in fuselage radii, level with its thickest section, at Mach 0, 0.6 and 0.8. At the fuselage's side it is 2.1 per cent at low speed and 2.5 at Mach 0.8; it falls only to two-thirds of that two radii out and a quarter at five — a long body's middle " + "spreads like a line of sources, not a point — and the section beside it is already running at twelve per cent over at low speed and twenty over at Mach 0.8. Ideal flow

A fuselage lowers its wing root's critical Mach number

A slender fuselage barely disturbs the air: two per cent of overspeed at its side, against the twelve a wing section of ordinary thickness makes. At the wing root the two are added, and two per cent on top of twelve moves the root's critical Mach number down by more than a hundredth — as much as making the whole wing thirteen per cent thicker. The fuselage's overspeed also fades far more slowly along the span than its size suggests, because the middle of a long body spreads its disturbance like a line, not a point.

 Area-preserving in the aorta, Murray's cube in the small arteries. The branching exponent k, in r_parent^k = r₁^k + r₂^k, that makes one junction reflect least of the heart's pulse, against the parent artery's radius, for a symmetric split and for side branches a half and 0.15 of the continuing trunk. In the aorta, where the pulse is carried by inertia, the transparent rule is close to 2 — area preserved — whatever the asymmetry. In arteries under a millimetre, where viscosity carries it, it is 3: Murray's law, the rule for the cheapest steady flow, is exactly the rule that passes the pulse. Asymmetry moves the answer only in between. Regimes and numbers

Murray's law passes the pulse where the pulse is viscous

The rule that makes an arterial junction transparent to the heart's pulse was an exponent, and real arteries do not split evenly: the aorta sheds side branches a fraction of its size and carries on. For a lopsided junction the transparent rule is still an exponent — the same one, exactly, while viscosity is negligible. With viscosity it is a single function of the parent's Womersley number: close to area-preserving in the aorta, and exactly Murray's cube in arteries under a millimetre, where the pulse moves as the steady flow does. The asymmetry matters only in between, and a lopsided tree reflects far less than an even one.

 Forced at the integral scale, the third moment nearly reaches four-fifths. The Kármán–Howarth balance at a Taylor-scale Reynolds number of 200, on the same model spectrum, for a flow forced in a band at the spectrum's peak and for one decaying. Each term is divided by (4/5)εr and plotted against separation in Kolmogorov lengths. The viscous term is the same for both. The forcing term is negligible until the separation approaches the integral scale, and −Dₗₗₗ/((4/5)εr) for the forced flow peaks at 0.965 at 90 Kolmogorov lengths, where the decaying flow's peaks at 0.747 at 32. Transition and turbulence

Forcing at the integral scale leaves the cascade alone

A decaying flow's third moment falls a quarter short of the four-fifths law at the Reynolds numbers a grid reaches. A flow forced at its largest scales, on the same spectrum at the same Reynolds number, falls short by three and a half per cent. The shortfall is not what a finite Reynolds number does to every flow; it is what the source does, and how fast it closes is set by how far the source reaches into the inertial range.

 Next to the body the gas remembers the nose. The gas temperature, over the free stream's, against distance from the axis of a hemisphere-nosed cylinder at Mach 15, at 2, 20 and 200 diameters behind the nose; the body's surface is at a half. The gas next to the body crossed the nearly normal part of the bow shock and carries its entropy: 16.7 times the free stream's temperature at 2 diameters, 9.29 at 200, falling outwards to the gas that crossed the weaker, oblique shock. The blast-wave analogy's core at 2 diameters, dashed, runs off the top of the frame on its way to infinity. Compressible flow

The gas beside a hypersonic body remembers its nose

The blast-wave analogy gets a blunt body's bow shock and afterbody pressure right and its temperature absurdly wrong: it puts the body in the empty core of an explosion, where the temperature has no bound. The real gas beside the body crossed the nearly normal shock at the nose and carries that crossing's entropy all the way down. Expanded to the afterbody's pressure, it is ten to twenty times the free stream's temperature at Mach 15, it never falls below a floor set by the nose alone, and the sheath that carries it is wider than the body.

 Over a day the breeze turns right round. The tip of the surface wind vector over one day, onshore to the right and along the coast upwards, at 15°, 30° and 45° north, with a spin-down time of twelve hours, in units of the push over the daily frequency. Without rotation the wind would swing on and off shore along one line. The Coriolis force turns it clockwise through the day into an ellipse; at 30°, where the Earth's inertial period is exactly a day, the turning keeps pace with the push and the ellipse is nearly a circle, of radius 1.8 against the ellipses' 1.2 at 15° and 1.2 at 45°. Ideal flow

At thirty degrees the Earth keeps time with the sea breeze

A sea breeze is Kelvin's circulation theorem failing: where warm air over land meets cool air over the sea, pressure and density surfaces cross and a circulation grows out of still air. Bjerknes' theorem prices the push, and the textbook's numbers give twenty-six metres a second in an hour — far more than any sea breeze blows. What stops it first is not friction but the evening: the push reverses before the wind can grow, and the day, not the drag, sets the breeze's size. Friction sets its hour, the Earth's rotation turns it through the day, and at thirty degrees, where the inertial period is a day, the turning keeps time with the push.

 Squeezed past closing, the tube is held open by its own fluid. The channel's half-width along one wavelength of a travelling squeeze that would push an empty tube's wall 1.3 half-widths inward — past the centreline — and the wall the squeeze and the fluid's pressure make together, for three compliances. The empty squeeze would overlap the centreline across a sixth of the wavelength; with fluid in the tube, the pressure that builds ahead of the narrowest point pushes the wall back, and the gap stays open at a hundredth to a tenth of the half-width. Flows and fields

A squeezed tube is held open by its own fluid

A peristaltic pump with a prescribed wall wave gets better the more its wave closes the channel, and at closure it becomes a piston. A real one squeezes an elastic wall and lets the fluid push back. Then the channel never closes: the pressure ahead of the narrowest point holds a gap open that grows as the square root of the wall's give, squeezing harder past closure pumps less, and the pump behaves as a displacement pump until a pressure of about one over its compliance blows the throat open — with an efficiency that stops short of one by an amount that grows with the wall's give.

All themes