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The thread: Taught wrongly, everywhere — page 23

Page 23 of 25, continuing through the 220 essays this motif runs through.

220 essays carry this thread — page 23 of 25.

With lift in proportion to spin, a drive gains from spin until its launch is level; the measured curves give it a best spin where drives are hit. The longest carry of a 70 m/s drive at each spin rate, its launch angle chosen for that spin, for four pairs of coefficients: lift in proportion to the spin ratio with fixed drag; drag rising with spin; lift growing as its 0.4 power; both measured forms together. The fixed pair peaks near 4,800 rpm, where its best launch reaches level, and drag rising alone near 4,400 rpm; lift saturating alone is still rising at 6,000; with both measured forms the carry peaks at 234.6 m at 2273 rpm and 16.8°. Fluids at work

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.

Over a swell the wing's lift swings further above its calm value than below it. The wing's lift coefficient through one encounter with a 50 m swell, heading into it at 50 m/s, for swells of amplitude 0.25, 0.5 and 0.7 m, with the calm sea's value. Phase zero is a crest under the leading edge. At 0.25 m it runs from 0.6 to 0.803, averaging 0.694. At 0.5 m it runs from 0.534 to 1, averaging 0.729. At 0.7 m it runs from 0.489 to 1.34, averaging 0.795. Calm, it is 0.684. One encounter takes 0.85 s. What is taught wrongly

A swell lifts a ground-effect wing more at its crests than it takes in its troughs

A wing skimming the sea gains its lift from the sea's reflection of it, and the reflection grows sharply as the gap closes. Over a swell the gap opens and closes with every wave, so the lift swings — further up at each crest than down at each trough, which raises the mean lift as well as shaking it. Climbing out of the swing is possible, but the height that calms the lift spends the cushion the craft was built for, and in a sea about two metres high it has spent nearly all of it.

Saddles that share one signal fold a cloud in a single step; independent saddles fold it steadily, and less. The share of a cloud seeded over the whole patch that has folded, against time, at a Stokes number of 0.16, in four seeded fields: with every saddle's strain the same signal, and with each saddle its own. After 400 time units the shared signal has folded 0.89, 0.89, 0.89, 0.89; the independent saddles 0.77, 0.85, 0.66, 0.69. A ninth of each cloud starts at a vortex centre, where the shared lattice holds it still. Flows and fields

A cloud folds where a saddle is strong, not when

When every saddle of a lattice strengthens and weakens together, a cloud of heavy particles folds in one step, at the strain's first strong excursion. Give each saddle its own random strength and the folding spreads out into a steady rate — and falls, because a particle now has to be at a saddle while that saddle is strong. The rate follows the Gaussian tail of the strain, at about a tenth of the time the strain spends past its fold condition, and a longer-lived strain helps only up to a few strain times.

A soft filter flies through most of the waves it is meant to follow, and follows them late. Against the encounter frequency over the crossover, for the ideal cut and the first- and second-order complementary pairs: left, the share of a wave's height the boat flies through rather than follows; right, how far the followed part lags the surface, in degrees. At the crossover itself the first-order pair flies through 0.707 of each wave and follows it 45° late; the second-order pair 1.22 and 90°. Fluids at work

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.

A quarter of the way into the layer, the lag follows the transitions along the chord. The transit lag a quarter of the way into the layer, as a multiple of the lag outside it, against chordwise station, at 0° and 4° on the thin cambered section at a chord Reynolds number of a million, with each surface's transition marked. At 0° the upper layer turns at 51% and the lower at 35%; the lag is −0.122 times the outside value at mid-chord and 0.61 at 95%. At 4° the upper layer turns at 11% and the lower not at all before the trailing edge; the lag is 2.91 times the outside value at mid-chord and 3.51 at 95%. What is taught wrongly

The side that turns turbulent first decides who arrives first near the wall

Inside a laminar layer the upper parcel's lead over the lower grows with depth. Real wings are not laminar to the trailing edge: one surface's layer turns turbulent first, and a turbulent layer is full almost to the wall. At the incidences a wing flies at, the upper side goes first and the exaggerated lead survives to the trailing edge, smaller than the laminar one and shrinking with the Reynolds number. Below about one degree the lower side goes first, and a tenth of the way into the layer the lower parcel arrives first.

Along the carry's ridge the run hardly moves the best spin, because every drive on it lands alike. The total distance of a 70 m/s drive, carry and run, at each spin rate launched at the angle that carries furthest for that spin, on a firm, a medium and a soft fairway, with the carry alone. The carry peaks at 234.6 m at 2273 rpm; the total along the ridge peaks at 1728 rpm on the firm turf, 274.3 m, 2052 rpm on the medium turf, 249.3 m, 2375 rpm on the soft turf, 239.9 m. Every drive on the ridge lands between 45.2° and 49.2°. Fluids at work

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.

On a flat bottom the plating's own give slows the water climbing it and takes a seventh off the slam; on a deep V, almost nothing. At the impact speed that loads the one-way panel to 200 MPa at each deadrise: left, the coupled panel's peak stress over the one-way panel's, against deadrise; right, the same against the panel's largest deflection over its rise across its width, w/(ℓ tan β). 4°: 2.27 m/s, ratio 0.847, deflection 3.99 mm; 6°: 2.9 m/s, ratio 0.894, deflection 4.24 mm; 8°: 3.44 m/s, ratio 0.934, deflection 4.44 mm; 10°: 3.94 m/s, ratio 0.972, deflection 4.61 mm; 15°: 4.99 m/s, ratio 1, deflection 4.81 mm; 20°: 5.8 m/s, ratio 0.983, deflection 4.69 mm. Ideal flow

Plating that gives way slows the water that slams it, but only on a flat bottom

The slamming pressure on a hull's bottom is a ridge that rides at the edge of the wetted width, and how fast that edge moves depends on how far the water has to climb. A panel of plating that bends inward under the load gives the water further to climb, and while it is moving away it slows the climb itself. Fed back into Wagner's condition, that takes a seventh off the peak stress of a panel on a four-degree bottom loaded to the edge of what aluminium can bear, and almost nothing on a deep V — because what matters is the plating's deflection against the bottom's own rise across the panel.

The body's dipole outshouts the flow's quadrupoles by one over the Mach number squared. The power of a wire's lift tone over the generous bound on its wake's quadrupole noise, against the wind's Mach number, for rms lift coefficients 0.2, 0.45 and 0.6 — the spread of the measurements. At Mach 0.03, a 10 m/s wind, the ratio is 9.4·10⁴; it falls as one over the Mach number squared and is still 104 at Mach 0.9, where a real cylinder's shedding has long since changed. Compressible flow

A wire sings with the force on it, not the flow round it

A free flow can only radiate as a quadrupole, four sources nearly cancelling, which is why a jet's noise grows as the eighth power of its speed and so little of its power becomes sound. Put a body in the flow and the cancellation is broken: the fluctuating force the body exerts is a dipole, its sound grows as the sixth power, and at the speed of any wind it outshouts the turbulence that made it by a factor of tens of thousands. The whistle of a wire is the force of its own wake, radiated.

Free in heave, the craft is an oscillator whose spring is its own cushion: it follows long swells and flies level over short ones. The craft's heave over the swell's amplitude against the encounter frequency over its own natural frequency, 2.07 rad/s with 0.69 of critical damping, for swells 30 to 800 m long; the curve is a linear oscillator driven through its spring with that damping. 30 m: 0.042 at 5.76; 50 m: 0.0972 at 3.58; 200 m: 0.723 at 1.03; 800 m: 1 at 0.324. What is taught wrongly

Free to rise and fall, a ground-effect craft rides its own cushion over the swell

A wing held still over a swell sees its gap change and its lift swing with it. A real ground-effect craft is not held: its weight sits on that lift, and ground effect, whose lift rises as the gap closes, gives it a height stiffness — a spring made of its own cushion — while its vertical speed changes its angle of attack and damps it. Free in heave it is an oscillator driven through that spring. Over long swells it follows the sea and keeps twice the held wing's clearance; over short ones it flies level and rides a dozen centimetres higher, because the cushion's swing is convex; and it comes closest to the crests over the swells it meets near its own natural frequency, never as close as the held wing does.

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