Every essay — page 7
Flows and fields Ideal flow Circulation and lift Viscosity Regimes and numbers Compressible flow Transition and turbulence Fluids at work What is taught wrongly Series Concepts Regimes Refutations Search
Fluids at work
Turbines, pipes, weirs, balls, sails, arteries and blades. What the conservation laws say about machines, which is more than a designer expects and less than a brochure claims.
Moody's fifth root is true at one size
A model pump is less efficient than the full-size machine, and since 1925 the gap has been bridged with a fifth root of the size ratio. Built from its losses, a pump's inefficiency scales three ways at once — leakage as the inverse size where a clearance cannot shrink, friction as a fifth root until the passages go rough, and a fixed share not at all — so the exponent runs from a third down to a twentieth, and the fifth root is right only near one size. The same arithmetic says a duty should be split by speed, not by width.
A drive's best spin falls where players hit it only because lift tires and drag grows
With lift in proportion to spin and drag fixed, a golf drive keeps gaining from backspin until its best launch has fallen to level, near 4,800 rpm, and past a few thousand more the model flies a ball the length of eight football pitches. Give lift and drag the curves wind tunnels measure — lift growing ever more slowly with the spin ratio, drag rising with it — and the best spin moves to near 2,300 rpm at 70 m/s, with a launch well above level, inside the range launch monitors recommend. Either curve alone leaves it at twice that or more. And along a ridge of best launches the carry hardly moves while the angle falls by ten degrees, which is why the launch angle is the softer of the two numbers.
A wand that lags its sea makes flying level the better bet
A foiling dinghy whose height control divides the sea sharply follows the long waves, flies level through the short and beats both pure strategies. Give the division the lag a real wand or filter has and the gain disappears in a moderate sea; in a rough one no crossover both keeps the foil under and spares it from pulling down. A second-order filter, which cuts more sharply, does worse rather than better, because it flies through more of the sea near its crossover than the sea contains.
The run moves the best drive below the ridge that carries furthest
A drive's carry is greatest along a ridge of launches on which more spin trades for a lower angle at almost no cost. Every drive on that ridge lands at about the same steep angle, so the run after landing hardly chooses between them. What the run rewards is leaving the ridge: less spin and a launch several degrees lower, a lower flight that lands flatter, gives up thirteen metres of carry and gets back twenty in the run. On an ordinary fairway the best drive in all lands near thirty-five degrees, at every ball speed; on a firm one the model's ground stops being a turf anybody has measured before the run stops paying.
The cheapest fork loses only its sideways speed, and pricing it closes the fork
A turbulent network built at least cost forks at 28.4°, with daughters three quarters of the parent's radius, and those numbers priced the pipes and never the split. Price the split as Borda priced a sudden widening and something exact appears: at the cheapest fork each daughter already runs at the parent's velocity component along it, so the junction loses nothing but the sideways part of the parent's speed, and its loss cannot be reduced by resizing the daughters. It can be reduced by narrowing the fork. A split costing under two per cent of the bill moves the cheapest angle by seven degrees, because the pipes' bill is flat at its best angle and the split's loss is not.
The layer every airway restarts bends Murray's cube towards the turbulent pipe's
A laminar fork does not lose energy the way a turbulent one does, in a burst of mixing at the split. It loses it all the way down each daughter, because the boundary layer starts again at every flow divider and an airway a few diameters long ends before the layer has grown across it. Pedley measured that extra dissipation in 1970, and in the form he wrote it the radius cancels: it depends on the flow and the length alone. Price it into the cheapest tree and Murray's cube law gives way to a flow growing as the radius to the power twelve-fifths or thirteen-fifths, the band the turbulent pipe's exponent sits in, across the first eleven generations of a resting lung.
A driver reaches the best drive only by striking upward
The longest drive asks for a launch near twelve degrees with little more than a thousand revolutions a minute of backspin, and a club cannot ask for those separately. Its strike sets the spin by the angle between the head's path and its face, and the launch by the face's loft, so a player who swings level can trade spin for launch only along one line — and that line misses the best drive. Striking upward moves the line. At a 45 m/s head speed the longest total comes at an attack of nine degrees upward with fourteen of loft, 4.6 metres past the best level strike, and it still lands near thirty-five degrees.
A bubble is throttled by its age, and a sheet by its length
A cavity cools the liquid it boils, and the cooling lowers the vapour pressure it needed. Whether that matters was a question about one number, the B-factor — vapour made over liquid cooled — and no real cavity's was known. Computed, the two kinds a pump has are nothing alike. A travelling bubble cools a thin shell that thins further as it stretches, so its B grows as the square root of its age and reaches the critical value at Brennen's thermal time: a millisecond in water at 60 °C, four microseconds at the boiling point. An attached sheet keeps renewing the liquid it cools, so its B is a few, fixed by its length and speed. In warm water the bubbles are suppressed forty degrees before the sheet.
A compressor needs one actuator for each way it can fail
A throttle alone cannot hold a compressor left of its peak in a large plenum: it has one degree of freedom and the machine has two ways to fail, and the throttle's own surge gain runs into a ceiling that the plenum's size does not move. Give the stall cell its own actuator — air injected at the rotor tips against the cell — and give the throttle a second signal, the flow, and a machine at B = 2 is held at ninety per cent of its peak flow, recovering from a kicked cell nearly three times the injector's capacity. Let the injection lag the cell by a radian and the line still holds, but almost no disturbance is survived.
Circulation and lift
Where lift actually comes from. The Kutta condition, the Joukowski aerofoil, and lift derived rather than assumed.
What actually holds a wing up
Not the shape, and not the story about air meeting up again behind. A wing lifts because there is circulation round it, and the sharp trailing edge is what decides how much.
The sharp edge decides
Ideal flow round a wing admits infinitely many solutions, each with a different lift, and all of them exact. One extra requirement — that the air leaves the trailing edge instead of whipping round it — picks a single one.
The lift curve, and why it is a straight line
Lift against angle of attack is a straight line, it does not pass through the origin, and its slope is very close to a number that has no business being there. All three facts fall out of the theory.