CHAPTER XIV.

USEFUL NOTES, TABLES, FORMULÆ, ETC.

§ 1. COMPARATIVE VELOCITIES.

Miles per hr. Feet per sec. Metres per sec.

10 = 14·7 = 4·470

15 = 22 = 6·705

20 = 29·4 = 8·940

25 = 36·7 = 11·176

30 = 44 = 13·411

35 = 51·3 = 15·646

§ 2. A metre = 39·37079 inches.

_In order to convert_:--

Metres into inches multiply by 39·37

" feet " 3·28

" yards " 1·09

" miles " 0·0006214

Miles per hour into ft. per min. multiply by 88·0

" min. " sec. " 88·0

" hr. into kilometres per hr. " 1·6093

" " metres per sec. " 0·44702

Pounds into grammes multiply by 453·593

" kilogrammes " 0·4536

§ 8. Total surface of a cylinder = circumference of base × height + 2

area of base.

Area of a circle = square of diameter × 0·7854.

Area of a circle = square of rad. × 3·14159.

Area of an ellipse = product of axes × 0·7854.

Circumference of a circle = diameter × 3·14159.

Solidity of a cylinder = height × area of base.

Area of a circular ring = sum of diameters × difference of diameters ×

0·7854.

For the area of a sector of a circle the rule is:--As 360 : number of

degrees in the angle of the sector :: area of the sector : area of

circle.

To find the area of a segment less than a semicircle:--Find the area

of the sector which has the same arc, and subtract the area of the

triangle formed by the radii and the chord.

The areas of corresponding figures are as the squares of corresponding

lengths.

§ 4. 1 mile = 1·609 kilometres.

1 kilometre = 1093 yards.

1 oz. = 28·35 grammes.

1 lb. = 453·59 "

1 lb. = 0·453 kilogrammes.

28 lb. = 12·7 "

112 lb. = 50·8 "

2240 lb. = 1016 "

1 kilogram = 2·2046 lb.

1 gram = 0·0022 lb.

1 sq. in. = 645 sq. millimetres.

1 sq. ft. = 0·0929 sq. metres.

1 sq. yard = 0·836 "

1 sq. metre = 10·764 sq. ft.

§ 5. One atmosphere = 14·7 lb. per sq. in. = 2116 lb. per sq. ft. =

760 millimetres of mercury.

A column of water 2·3 ft. high corresponds to a pressure of 1 lb. per

sq. in.

1 H.P. = 33,000 ft.-lb. per min. = 746 watts.

Volts × amperes = watts.

{pi} = 3·1416. _g_ = 32·182 ft. per sec. at London.

§ 6. TABLE OF EQUIVALENT INCLINATIONS.

Rise. Angle in Degs.

1 in 30 1·91

1 " 25 2·29

1 " 20 2·87

1 " 18 3·18

1 " 16 3·58

1 " 14 4·09

1 " 12 4·78

1 " 10 5·73

1 " 9 6·38

1 " 8 7·18

1 " 7 8·22

1 " 6 9·6

1 " 5 11·53

1 " 4 14·48

1 " 3 19·45

1 " 2 30·00

1 " {square root}2 45·00

§ 7. TABLE OF SKIN FRICTION.

Per sq. ft. for various speeds and surface lengths.

-----------------+-------------+-------------+-------------+------------

Velocity of Wind | 1 ft. Plane | 2 ft. Plane | 4 ft. Plane | 8 ft. Plane

-----------------+-------------+-------------+-------------+------------

10 | ·00112 | ·00105 | ·00101 | ·000967

15 | ·00237 | ·00226 | ·00215 | ·00205

20 | ·00402 | ·00384 | ·00365 | ·00349

25 | ·00606 | ·00579 | ·00551 | ·00527

30 | ·00850 | ·00810 | ·00772 | ·00736

35 | ·01130 | ·0108 | ·0103 | ·0098

-----------------+-------------+-------------+-------------+------------

This table is based on Dr. Zahm's experiments and the equation

_f_ = 0·00000778_l_^{-0·07}_v_^{1·85}

Where _f_ = skin friction per sq. ft.; _l_ = length of surface; _v_ =

velocity in feet per second.

In a biplane model the head resistance is probably from twelve to

fourteen times the skin friction; in a racing monoplane from six to

eight times.

§ 8. TABLE I.--(METALS).

--------------+------------+-----------------+-------------

Material | Specific | Elasticity E[A] | Tenacity

| Gravity | | per sq. in.

--------------+------------+-----------------+-------------

Magnesium | 1·74 | | {22,000-

| | | {32,000

Magnalium[B] | 2·4-2·57 | 10·2 |

Aluminium- } | | |

Copper[C]} | 2·82 | | 54,773

Aluminium | 2·6 | 11·1 | 26,535

Iron | 7·7 (about)| 29 | 54,000

Steel | 7·8 (about)| 32 | 100,000

Brass | 7·8-8·4 | 15 | 17,500

Copper | 8·8 | 36 | 33,000

Mild Steel | 7·8 | 30 | 60,000

| | |

--------------+------------+-----------------+-------------

[A] E in millions of lb. per sq. in.

[B] Magnalium is an alloy of magnesium and aluminium.

[C] Aluminium 94 per cent., copper 6 per cent. (the best

percentage), a 6 per cent. alloy thereby doubles the

tenacity of pure aluminium with but 5 per cent.

increase of density.

--------------+------------+-----------------+-------------

§ 9. TABLE II.--WIND PRESSURES.

_p_ = _kv²_.

_k_ coefficient (mean value taken) ·003 (miles per hour) = 0·0016 ft.

per second. _p_ = pressure in lb. per sq. ft. _v_ = velocity of wind.

Miles per hr. Ft. per sec. Lb. per sq. ft.

10 14·7 0·300

12 17·6 0·432

14 20·5 0·588

16 23·5 0·768

18 26·4 0·972

20 29·35 1·200

25 36·7 1·875

30 43·9 2·700

35 51·3 3·675

§ 10. Representing normal pressure on a plane surface by 1; pressure

on a rod (round section) is 0·6; on a symmetrical elliptic cross

section (axes 2:1) is 0·2 (approx.). Similar shape, but axes 6:1, and

edges sharpened (_see_ ch. ii., § 5), is only 0·05, or 1/20, and for

the body of minimum resistance (_see_ ch. ii., § 4) about 1/24.

§ 11. TABLE III.--LIFT AND DRIFT.

On a well shaped aerocurve or correctly designed cambered surface.

Aspect ratio 4·5.

Inclination. Ratio Lift to Drift.

0° 19:1

2·87° 15:1

3·58° 16:1

4·09° 14:1

4·78° 12:1

5·73° 9·6:1

7·18° 7·9:1

Wind velocity 40 miles per hour. (The above deduced from some

experiments of Sir Hiram Maxim.)

At a velocity of 30 miles an hour a good aerocurve should lift 21 oz.

to 24 oz. per sq. ft.

§ 12. TABLE IV.--LIFT AND DRIFT.

On a plane aerofoil.

N = P(2 sin {alpha}/1 + sin² {alpha})

Inclination. Ratio Lift to Drift.

1° 58·3:1

2° 29·2:1

3° 19·3:1

4° 14·3:1

5° 11·4:1

6° 9·5:1

7° 8·0:1

8° 7·0:1

9° 6·3:1

10° 5·7:1

P = 2_kd_ AV² sin {alpha}.

A useful formula for a single plane surface. P = pressure supporting

the plane in pounds per square foot, _k_ a constant = 0·003 in miles

per hour, _d_ = the density of the air.

A = the area of the plane, V relative velocity of translation through

the air, and {alpha} the angle of flight.

Transposing we have

AV² = P/(2_kd_ sin {alpha})

If P and {alpha} are constants; then AV² = a constant or area is

inversely as velocity squared. Increase of velocity meaning diminished

supporting surface (_and so far as supporting surface goes_), diminished

resistance and skin friction. It must be remembered, however, that while

the work of sustentation diminishes with the speed, the work of

penetration varies as the cube of the speed.

§ 13. TABLE V.--TIMBER.

Column Headings:

A. Material

B. Specific Gravity

C. Weight per Cub. Ft. in Lb.

D. Strength per Sq. In. in Lb.

E. Ultimate Breaking Load (Lb.) span 1' x 1" x 1"

F. Relative Resilience in Bending

G. Modulus of Elasticity in millions of Lb. per Sq. In. for Bending

H. Relative Value. Bending Strength compared with Weight

---------------+-----+-------+-------------+-------+-----+-----+----

A |B | C | D |E |F |G | H

---------------+-----+-------+-------------+-------+-----+-----+----

Ash | ·79 | 43-52 |14,000-17,000| 622 |4·69 |1·55 |13·0

Bamboo | | 25[A]| 6300[53] | |3·07 |3·20 |

Beech | ·69 | 43 |10,000-12,000| 850 | |1·65 |19·8

Birch | ·71 | 45 | 15,000 | 550 | |3·28 |12·2

Box |1·28 | 80 |20,000-23,000| 815 | | |10·2

Cork | ·24 | 15 | | | | |

Fir (Norway | | | | | | |

Spruce) | ·51 | 32 | 9,000-11,000| 450 |3·01 |1·70 |14·0

American | | | | | | |

Hickory | | 49 | 11,000 | 800 |3·47 |2·40 |16·3

Honduras | | | | | | |

Mahogany | ·56 | 35 | 20,000 | 750 |3·40 |1·60 |21·4

Maple | ·68 | 44 | 10,600 | 750 | | |17·0

American White | | | | | | |

Pine | ·42 | 25 | 11,800 | 450 |2·37 |1·39 |18·0

Lombardy Poplar| | 24 | 7,000 | 550 |2·89 | 0·77|22·9

American Yellow| | | | | | |

Poplar | | 44 | 10,000 | |3·63 |1·40 |

Satinwood | ·96 | 60 | |1,033 | | |17·2

Spruce | ·50 | 31 | 12,400 | 450 | | |14·5

Tubular Ash, | | | | | | |

_t_ = 1/8 _d_ | | 47 | | |3·50 |1·55 |

---------------+-----+-------+-------------+-------+-----+-----+----

_t_ = thickness: _d_ = diameter.

[A] Given elsewhere as 55 and 22,500 (_t_ = 1/3_d_), evidently

regarded as solid.

§ 14.--=Formula connecting the Weight Lifted in Pounds per Square Foot

and the Velocity.=--The empirical formula

W = (V²C)/_g_

Where W = weight lifted in lb. per sq. ft.

V = velocity in ft. per sec.

C = a constant = 0·025.

_g_ = 32·2, or 32 approx.

may be used for a thoroughly efficient model. This gives

(approximately)

1 lb. per sq. ft. lift at 25 miles an hour.

21 oz. " " 30 "

6 oz. " " 15 "

4 oz. " " 12 "

2·7 oz. " " 10 "

Remember the results work out in feet per second. To convert

(approximately) into miles per hour multiply by 2/3.

§ 15. =Formula connecting Models of Similar Design, but Different

Weights.=

D {proportional to} {square root}W.

or in models of _similar design_ the distances flown are proportional

to the square roots of the weights. (Derived from data obtained from

Clarke's flyers.)

For models from 1 oz. to 24-30 oz. the formula appears to hold very

well. For heavier models it appears to give the heavier model rather

too great a distance.

Since this was deduced a 1 oz. Clarke model of somewhat similar design

but longer rubber motor has flown 750 ft. at least; it is true the

design is not, strictly speaking, similar, but not too much reliance

must be placed on the above. The record for a 1 oz. model to date is

over 300 yards (with the wind, of course), say 750 ft. in calm air.

§ 16. =Power and Speed.=--The following formula, given by Mr. L. Blin

Desbleds, between these is--

W/W{0} = (3_v{0}_)/(4_v_) + ¼(_v_/_v{0}_)³.

Where _v{0}_ = speed of minimum power

W{0} = work done at speed _v{0}_.

W = work done at speed _v_.

Making _v_ = 2_v{0}_, i.e. doubling the speed of minimum power, and

substituting, we have finally

W = (2-3/8)W{0}

i.e. the speed of an aeroplane can be doubled by using a power 2-3/8

times as great as the original one. The "speed of minimum power" being

the speed at which the aeroplane must travel for the minimum

expenditure of power.

§ 17. The thrust of the propeller has evidently to balance the

Aerodynamic resistance = R

The head resistance (including skin friction) = S

Now according to Renard's theorem, the power absorbed by R + S is a

minimum when

S = R/3.

Having built a model, then, in which the total resistance

= (4/3)R.

This is the thrust which the propeller should be designed to give. Now

supposing the propeller's efficiency to be 80 per cent., then P--the

minimum propulsion power

= (4/3)R × 100/80 × 100/75 × _v_.

Where 25 per cent. is the slip of the screw, _v_ the velocity of the

aeroplane.

§ 18. =To determine experimentally the Static Thrust of a

Propeller.=--Useful for models intended to raise themselves from the

ground under their own power, and for helicopters.

The easiest way to do this is as follows: Mount the propeller on the

shaft of an electric motor, of sufficient power to give the propeller

1000 to 1500 revolutions per minute; a suitable accumulator or other

source of electric energy will be required, a speedometer or speed

counter, also a voltmeter and ammeter.

Place the motor in a pair of scales or on a suitable spring balance

(the former is preferable), the axis of the motor vertical, with the

propeller attached. Rotate the propeller so that the air current is

driven _upwards_. When the correct speed (as indicated by the speed

counter) has been attained, notice the difference in the readings if a

spring balance be used, or, if a pair of scales, place weights in the

scale pan until the downward thrust of the propeller is exactly

balanced. This gives you the thrust in ounces or pounds.

Note carefully the voltage and amperage, supposing it is 8 volts and

10 amperes = 80 watts.

Remove the propeller and note the volts and amperes consumed to run

the motor alone, i.e. to excite itself, and overcome friction and air

resistance; suppose this to be 8 volts and 2 amperes = 16; the

increased load when the propeller is on is therefore

80 - 16 = 64 watts.

All this increased power is not, however, expended on the propeller.

The lost power in the motor increases as C²R.

R = resistance of armature and C = current. If we deduct 10 per cent.

for this then the propeller is actually driven by 56 watts.

Now 746 watts = 1 h.p.

{therefore} 56/746 = 1/13 h.p. approx.

at the observed number of revolutions per minute.

§ 19. N.B.--The h.p. required to drive a propeller varies as the cube

of the revolutions.

_Proof._--Double the speed of the screw, then it strikes the air twice

as hard; it also strikes twice as much air, and the motor has to go

twice as fast to do it.

§ 20. To compare one model with another the formula

Weight × velocity (in ft. per sec.)/horse-power

is sometimes useful.

§ 21. =A Horse-power= is 33,000 lb. raised one foot in one minute, or

550 lb. one foot in one second.

A clockwork spring raised 1 lb. through 4½ ft. in 3 seconds. What

is its h.p.?

1 lb. through 4½ ft. in 3 seconds

is 1 lb. " 90 ft. " 1 minute.

{therefore} Work done is 90 ft.-lb.

= 90/33000 = 0·002727 h.p.

The weight of the spring was 6¾ oz. (this is taken from an actual

experiment), i.e. this motor develops power at the rate of 0·002727

h.p. for 3½ seconds only.

§ 22. =To Ascertain the H.P. of a Rubber Motor.= Supposing a propeller

wound up to 250 turns to run down in 15 seconds, i.e. at a mean speed

of 1200 revolutions per minute or 20 per second. Suppose the mean

thrust to be 2 oz., and let the pitch of the propeller be 1 foot. Then

the number of foot-pounds of energy developed

= (2 oz. × 1200 revols. × 1 ft. (pitch)) / 16 oz.

= 150 ft.-lb. per minute.

But the rubber motor runs down in 15 seconds.

{therefore} Energy really developed is

= (150 × 15) / 60 = 37·5 ft.-lb.

The motor develops power at rate of 150/33000 = 0·004545 h.p., but for

15 seconds only.

§ 23. =Foot-pounds of Energy in a Given Weight of Rubber=

(experimental determination of).

Length of rubber 36 yds.

Weight " 2-7/16 oz.

Number of turns = 200.

12 oz. were raised 19 ft. in 5 seconds.

i.e. ¾ lb. was raised 19 × 12 ft. in 1 minute.

i.e. 1 lb. was raised 19 × 3 × 3 ft. in 1 minute.

= 171 ft. in 1 minute.

i.e. 171 ft.-lb. of energy per minute. But actual time was 5 seconds.

{therefore} Actual energy developed by 2-7/16 oz. of rubber of 36

yards, i.e. 36 strands 1 yard each at 200 turns is

= 171/12 ft.-lb.

= 14¼ ft.-lb.

This allows nothing for friction or turning the axle on which the cord

was wound. Ball bearings were used; but the rubber was not new and

twenty turns were still unwound at the end of the experiment. Now

allowing for friction, etc. being the same as on an actual model, we

can take ¾ of a ft.-lb. for the unwound amount and estimate the

total energy as 15 ft.-lb. as a minimum. The energy actually developed

being at the rate of 0·0055 h.p., or 1/200 of a h.p. if supposed

uniform.

§ 24. The actual energy derivable from 1 lb. weight of rubber is

stated to be 300 ft.-lb. On this basis 2-7/16 oz. should be capable of

giving 45·7 ft.-lb. of energy, i.e. three times the amount given

above. Now the motor-rubber not lubricated was only given 200

turns--lubricated 400 could have been given it, 600 probably before

rupture--and the energy then derivable would certainly have been

approximating to 45 ft.-lb., i.e. 36·25. Now on the basis of 300

ft.-lb. per lb. a weight of ½ oz. (the amount of rubber carried in

"one-ouncers") gives 9 ft.-lb. of energy. Now assuming the gliding

angle (including weight of propellers) to be 1 in 8; a perfectly

efficient model should be capable of flying eight times as great a

distance in a horizontal direction as the energy in the rubber motor

would lift it vertically. Now 9 ft.-lb. of energy will lift 1 oz. 154

ft. Therefore theoretically it will drive it a distance (in yards) of

(8 × 154)/3 = 410·6 yards.

Now the greatest distance that a 1 oz. model has flown in perfectly

calm air (which never exists) is not known. Flying with the wind 500

yards is claimed. Admitting this what allowance shall we make for the

wind; supposing we deduct half this, viz. 250 yards. Then, on this

assumption, the efficiency of this "one ouncer" works out (in

perfectly still air) at 61 per cent.

The gliding angle assumption of 1 in 8 is rather a high one, possibly

too high; all the writer desires to show is the method of working out.

Mr. T.W.K. Clarke informs me that in his one-ouncers the gliding

angle is about 1 in 5.

§ 25. =To Test Different Motors or Different Powers of the Same Kind

of Motor.=--Test them on the same machine, and do not use different

motors or different powers on different machines.

§ 26. =Efficiency of a Model.=--The efficiency of a model depends on

the weight carried per h.p.

§ 27. =Efficiency of Design.=--The efficiency of some particular

design depends on the amount of supporting surface necessary at a

given speed.

§ 28. =Naphtha Engines=, that is, engines made on the principle of the

steam engine, but which use a light spirit of petrol or similar agent

in their generator instead of water with the same amount of heat, will

develop twice as much energy as in the case of the ordinary steam

engine.

§ 29.=Petrol Motors.=

Horse-power. No. of Cylinders. Weight.

¼ Single 4½ lb.

½ to ¾ " 6½ "

1½ Double 9 "

§ 30. =The Horse-power of Model Petrol Motors.=--Formula for rating of

the above.

(R.P.M. = revolutions per minute.)

H.P. = ((Bore)² × stroke × no. of cylinders × R.P.M.)/12,000

If the right-hand side of the equation gives a less h.p. than that

stated for some particular motor, then it follows that the h.p. of the

motor has been over-estimated.

[Illustration: FIG. 56.]

§ 30A. =Relation between Static Thrust of Propeller and Total Weight

of Model.=--The thrust should be approx. = ¼ of the weight.

§ 31. =How to find the Height of an Inaccessible Object by Means of

Three Observations taken on the Ground (supposed flat) in the same

Straight Line.=--Let A, C, B be the angular elevations of the object

D, as seen from these points, taken in the same straight line. Let the

distances B C, C A and A B be _a_, _b_, _c_ respectively. And let

required height P D = _h_; then by trigonometry we have (see Fig. 56)

_h²_ = _abc_/(_a_ cot²A - _c_ cot²C + _b_ cot²B).

§ 32. =Formula= for calculating the I.H.P. (indicated horse-power) of

a single-cylinder double-acting steam-engine.

Indicated h.p. means the h.p. actually exerted by the steam in the

cylinder without taking into account engine friction. Brake h.p. or

effective h.p. is the actual h.p. delivered by the crank shaft of the

engine.

I.H.P. = (2 × S × R × A × P)/33,000.

Where S = stroke in feet.

R = revolutions per minute.

A = area of piston in inches.

P = mean pressure in lb. exerted per sq. in. on the piston.

The only difficulty is the mean effective pressure; this can be found

approximately by the following rule and accompanying table.

TABLE VI.

---------+----------+---------+----------+---------+---------

Cut-off | Constant | Cut-off | Constant | Cut-off | Constant

---------+----------+---------+----------+---------+---------

1/6 | ·566 | 3/8 | ·771 | 2/3 | ·917

1/5 | ·603 | ·4 | ·789 | ·7 | ·926

1/4 | ·659 | 1/2 | ·847 | 3/4 | ·937

·3 | ·708 | ·6 | ·895 | ·8 | ·944

1/3 | ·743 | 5/8 | ·904 | 7/8 | ·951

---------+----------+---------+----------+---------+---------

Rule.--"Add 14·7 to gauge pressure of boiler, this giving 'absolute

steam pressure,' multiply this sum by the number opposite the fraction

representing the point of cut-off in the cylinder in accompanying

table. Subtract 17 from the product and multiply the remainder by 0·9.

The result will be very nearly the M.E.P." (R.M. de Vignier.)

FOOTNOTE:

[53] Given elsewhere as 55 and 22,500 (_t_ = 1/3 _d_), evidently

regarded as solid.

APPENDIX A.

SOME MODELS WHICH HAVE WON MEDALS AT OPEN COMPETITIONS.

[Illustration: FIG. 57.--THE G.P.B. SMITH MODEL.]

The model shown in Fig. 57 has won more competition medals than any

other. It is a thoroughly well designed[54] and well constructed

model. Originally a very slow flyer, the design has been simplified,

and although by no means a fast flyer, its speed has been much

accelerated. Originally a one-propeller machine, it has latterly been

fitted with twin propellers, with the idea of obtaining more

directional control; but in the writer's opinion, speaking from

personal observation, with but little, if any, success. The steering

of the model is effected by canting the elevator. Originally the

machine had ailerons for the purpose, but these were removed owing, I

understand, to their retarding the speed of the machine.

In every competition in which this machine has been entered it has

always gained very high marks for stability.

[Illustration: FIG. 58.--THE GORDON-JONES DIHEDRAL BIPLANE.]

Up to the time of writing it has not been provided with anything in

the nature of fins or rudder.

Fig. 58 is a biplane very much after the type of the model just

alluded to, but the one straight and one curved aerofoil surfaces are

here replaced by two parallel aerofoils set on a dihedral angle. The

large size of the propeller should be noted; with this the writer is

in complete agreement. He has not unfortunately seen this model in

actual flight.

The scientifically designed and beautifully made models illustrated in

Fig. 59 are so well known that any remarks on them appear

superfluous. Their efficiency, so far as their supporting area goes,

is of the highest, as much as 21 oz. per square foot having been

carried.

[Illustration: FIG. 59.--MESSRS. T.W.K. CLARKE AND CO.'S MODEL

FLYERS.]

For illustrations, etc., of the Fleming-Williams model, _see_ ch. v.,

§ 23.

(Fig. 60.) This is another well-constructed and efficient model, the

shape and character of the aerofoil surfaces much resembling those of

the French toy monoplane AL-MA (see § 4, ch. vii.), but they are

supported and held in position by quite a different method, a neat

little device enabling the front plane to become partly detached on

collision with any obstacle. The model is provided with a keel (below

the centre of gravity), and rudder for steering; in fact, this machine

especially claims certainty of directional control. The writer has

seen a number of flights by this model, but it experiences, like other

models, the greatest difficulty in keeping straight if the conditions

be adverse.

The model which will do this is, in his opinion, yet to be evolved.

The small size of the propellers is, of course, in total disagreement

with the author's ideas. All the same, the model is in many respects

an excellent one, and has flown over 300 yards at the time of writing.

[Illustration: FIG. 60.--THE DING SAYERS MONOPLANE.]

More than a year ago the author made a number of models with

triangular-shaped aerofoils, using umbrella ribs for the leading edge

and steel piano wire for the trailing, but has latterly used aerofoils

of the elongated ellipse shape.

Fig. 61 is an illustration of one of the author's latest models which

won a Bronze Medal at the Long Distance Open Competition, held at the

Crystal Palace on July 27, 1910, the largest and most keenly contested

competition held up to that date.

The best and straightest flight against the wind was made by this

model.

On the morning of the competition a flight of about 320 yards

(measured in a straight line) was made on Mitcham Common, the model

being launched against the wind so as to gain altitude, and then

flying away with the breeze behind the writer. Duration of flight 50

seconds. The following are the chief particulars of the

model:--Weight, 7½ oz. Area of supporting surface, 1-1/3 sq. ft.

Total length, 4 ft. Span of main aerofoil, 25 in. Aspect ratio, 4 : 1.

Diameter of propeller, 14 in. Two strand geared rubber motor, carrying

altogether 28 strands of 1/16 square rubber cord 43 in. long. The

propeller was originally a Venna, but with the weight reduced by

one-third, and considerable alteration made in its central contours.

The front skid of steel pianoforte wire, the rear of jointless cane

wire tipped; the rear skid was a necessity in order to protect the

delicate gearing mechanism, the weight of which was reduced to a

minimum.

[Illustration: FIG. 61.--THE AUTHOR'S "GRASSHOPPER" MODEL.]

The very large diameter of the propeller should be noted, being 56

per cent. of the span. The fin, high above the centre of gravity, was

so placed for transverse stability and direction. At the rear of the

fin was a rudder. The small amount of rubber carried (for a long

distance machine) should also be noted, especially when allowing for

friction in gearing, etc.

The central rod was a penny bamboo cane, the large aerofoil of

jointless cane and Hart's fabric, and the front aerofoil of steel wire

surfaced with the same material.

LONDON: PRINTED BY WILLIAM CLOWES AND SONS, LIMITED, GREAT WINDMILL

STREET, W., AND DUKE STREET, STAMFORD STREET, S.E.

FOOTNOTE:

[54] The design is patented.

_October, 1910_

A SHORT LIST OF

SCIENTIFIC BOOKS

PUBLISHED AND SOLD BY

E. & F.N. SPON, Limited,

57 Haymarket, London, S.W.

SOLE ENGLISH AGENTS for the Books of--

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PAGE

AERONAUTICS 2

AGRICULTURE 2

ARCHITECTURE 3

ARTILLERY 5

BRIDGES AND ROOFS 5

BUILDING 3

CEMENT AND CONCRETE 7

CIVIL ENGINEERING 8

DICTIONARIES 11

DOMESTIC ECONOMY 12

DRAWING 13

ELECTRICAL ENGINEERING 14

FOREIGN EXCHANGE 19

GAS AND OIL ENGINES 20

GAS LIGHTING 20

HISTORICAL; BIOGRAPHICAL 21

HOROLOGY 22

HYDRAULICS 22

INDUSTRIAL CHEMISTRY 24

IRRIGATION 27

LOGARITHM TABLES 28

MANUFACTURES 24

MARINE ENGINEERING 28

MATERIALS 30

MATHEMATICS 31

MECHANICAL ENGINEERING 33

METALLURGY 36

METRIC TABLES 38

MINERALOGY AND MINING 38

MUNICIPAL ENGINEERING 45

NAVAL ARCHITECTURE 28

ORGANISATION 40

PHYSICS 41

PRICE BOOKS 42

RAILWAY ENGINEERING 43

SANITATION 45

STRUCTURAL DESIGN 45

TELEGRAPH CODES 47

WARMING; VENTILATION 47

WATER SUPPLY 48

WORKSHOP PRACTICE 49

USEFUL TABLES 52

MISCELLANEOUS 53

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AERONAUTICS

=The Atmosphere=: its characteristics and dynamics. By F.J.B.

CORDEIRO. With 35 illus. 129 pp. medium 8vo. (_New York, 1910_)

_net_ 10 6

=Theory and Practice of Model Aeroplaning.= By V.E. JOHNSON. 61

illus. 150 pp. crown 8vo. (_1910_)

_net_ 3 6

=How to Build a 20-ft. Biplane Glider.= By A.P. MORGAN. 31

illus. 60 pp. crown 8vo, limp. (S. & C. SERIES, NO. 14.) (_New

York, 1909_)

_net_ 1 6

=Flight-Velocity.= By A. SAMUELSON. 4 plates, 42 pp. 8vo,

sewed. (_1906_)

_net_ 2 0

=Resistance of Air and the Question of Flying.= By A.

SAMUELSON. 23 illus. 36 pp. 8vo, sewed. (_1905_)

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AGRICULTURE.

=Hemp.= A Practical Treatise on the Culture for Seed and Fibre.

By S.S. BOYCE. 13 illus. 112 pp. crown 8vo. (_New York, 1900_)

_net_ 2 0

=The Fertilisation of Tea.= By G.A. COWIE. With 17 illus. 68

pp. crown 8vo, sewed. (_1908_)

_net_ 2 6

=Farm Drainage.= By H.F. FRENCH. 100 illus. 284 pp. crown 8vo.

(_New York, 1904_)

_net_ 4 6

=Talks on Manures.= By J. HARRIS. New edition, 366 pp. crown

8vo. (_New York, 1893_)

_net_ 6 6

=Coffee=, its Culture and Commerce in all Countries. By C.G.W.

LOCK. 11 plates, 274 pp. crown 8vo. (_1888_)

12 6

=Sugar, a Handbook for Planters and Refiners.= By the late J.A.

R. NEWLANDS and B.E.R. NEWLANDS. 236 illus. 876 pp. demy 8vo.

(_London, 1909_)

_net_ 1 5 0

=Hops=, their Cultivation, Commerce and Uses. By P.L. SIMMONDS.

143 pp. crown 8vo. (_1877_)

4 6

=The Future of Cocoa-Planting=. By H. HAMEL SMITH. With

illustrations, 95 pp. crown 8vo, sewed. (_1908_)

_net_ 1 0

=Estate Fences=, their Choice, Construction and Cost. By A.

VERNON. Re-issue, 150 illus. 420 pp. 8vo. (_1909_)

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ARCHITECTURE AND BUILDING.

=The Hydropathic Establishment and its Baths.= By R.O. ALLSOP.

8 plates, 107 pp. demy 8vo. (_1891_)

5 0

=The Turkish Bath=, its Design and Construction. By R.O.

ALLSOP. 27 illus. 152 pp. demy 8vo. (_1890_)

6 0

=Public Abattoirs=, their Planning, Design and Equipment. By

R.S. AYLING. 33 plates, 100 pp. demy 4to. (_1908_)

_net_ 8 6

=The Builder's Clerk.= By T. BALES. Second edition, 92 pp.

fcap. 8vo. (_1904_)

1 6

=Glossary of Technical Terms= used in Architecture and the

Building Trades. By G.J. BURNS. 136 pp. crown 8vo. (_1895_)

3 6

=Chimney Design and Theory.= By W.W. CHRISTIE. Second edition,

54 illus. 200 pp. crown 8vo. (_New York, 1902_)

_net_ 12 6

=Approximate Estimates.= By T.E. COLEMAN. Third edition, 481

pp. oblong 32mo, leather. (_1907_)

_net_ 5 0

=Stable Sanitation and Construction.= By T.E. COLEMAN. 183

illus. 226 pp. crown 8vo. (_1897_)

_net_ 6 0

=Architectural Examples= in Brick, Stone, Wood and Iron. By W.

FULLERTON. Third edition, 245 plates, 254 pp. demy 4to.

(_1908_)

_net_ 15 0

=Bricklaying System.= By F.B. GILBRETH. Fully illustrated, 321

pp. 8vo. (_New York, 1909_)

_net_ 12 6

=Field System.= By F.B. GILBRETH. 194 pp. 12mo leather. (_New

York, 1908_)

_net_ 12 6

=The Building Trades Pocket Book.= Compiled by R. HALL. 12mo.

With interchangeable diary

_net_ 1 6

Ditto ditto, in leather

_net_ 2 6

=The Clerk of Works' Vade Mecum.= By G.G. HOSKINS. Seventh

edition, 52 pp. fcap. 8vo. (_1901_)

1 6

=A Handbook of Formulæ, Tables, and Memoranda=, for

Architectural Surveyors and others engaged in Building. By J.T.

HURST. Fifteenth edition, 512 pp. royal 32mo, roan. (_1905_)

_net_ 5 0

=Quantity Surveying=, for the Use of Surveyors, Architects,

Engineers and Builders. By J. LEANING. Fifth edition, 936 pp.

demy 8vo. (_1904_)

_net_ 1 5 0

=Obstruction to Light.= A Graphic Method of determining

Problems of Ancient Lights. By H.B. MOLESWORTH. 9 folding

plates, 4to. (_1902_)

_net_ 6 0

=Suburban Houses.= A series of practical plans. By J.H.

PEARSON. 46 plates and 12 pp. text, crown 4to. (_1905_)

_net_ 7 6

=Solid Bitumens=, their Physical and Chemical Properties and

Chemical Analysis. By S.F. PECKHAM. 23 illus. 324 pp. 8vo.

(_New York, 1909_)

_net_ 1 1 0

=Roman Architecture, Sculpture and Ornament.= By G.B. PIRANESI.

200 plates, reproduced in facsimile from the original. 2 vols.

Imperial folio, in wrappers. (_1900_)

_net_ 2 2 0

=The Seven Periods of English Architecture=, defined and

illustrated. By E. SHARPE. Third edition, 20 steel plates,

royal 8vo. (_1888_)

12 6

=Our Factories, Workshops and Warehouses=, their Sanitary and

Fire-Resisting Arrangements. By B.H. THWAITE. 183 illus. 282

pp. crown 8vo. (_1882_)

9 0

=Elementary Principles of Carpentry.= By T. TREDGOLD and J.T.

HURST. Eleventh edition, 48 plates, 517 pp. crown 8vo. (_1904_)

12 6

=Practical Stair Building and Handrailing.= By W.H. WOOD. 32

plates, 91 pp. crown 4to. (_1894_)

10 6

=Spons' Architects' and Builders' Pocket Price-Book=,

Memoranda, Tables and Prices. Edited by CLYDE YOUNG. Revised by

STANFORD M. BROOKS. Illustrated, 552 pp. 16mo, leather cloth

(size 6½ in. by 3¾ in. by ½ in. thick). Issued annually

_net_ 3 0

=Heating Engineers' Quantities.= By W.L. WHITE and G.M. WHITE.

4 plates, 33 pp. folio. (_1910_)

_net_ 10 6

ARTILLERY.

=Guns and Gun Making Material.= By G. EDE. Crown 8vo. (_1889_)

6 0

=Treatise on Application of Wire to Construction of Ordnance.=

By J.A. LONGRIDGE. 180 pp. 8vo. (_1884_)

1 5 0

=The Progress of Artillery: Naval Guns.= By J.A. LONGRIDGE.

8vo, sewed. (_1896_)

2 0

=The Field Gun of the Future.= By J.A. LONGRIDGE. 8vo, sewed.

(_1892_)

2 6

BRIDGES, ARCHES, ROOFS, AND STRUCTURAL DESIGN.

=Strains in Ironwork.= By HENRY ADAMS. Fourth edition, 8 plates, 65

pp. crown 8vo. (_1904_)

5 0

=The Practical Designing of Structural Ironwork.= By HENRY ADAMS. 13

plates, 194 pp. 8vo. (_1894_)

8 6

=Designing Ironwork.= By HENRY ADAMS. Second series. 8vo, sewed.

Part I. A Steel Box Girder. (_1894_)

_net_ 0 9

" II. Built-up Steel Stanchions. (_1901_)

_net_ 1 3

" III. Cisterns and Tanks. (_1902_)

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" IV. A Fireproof Floor. (_1903_)

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=A Practical Treatise on Segmental and Elliptical Oblique or Skew

Arches.= By G.J. BELL. Second edition, 17 plates, 125 pp. royal 8vo.

(_1906_)

_net_ 1 1 0

=Economics of Construction in relation to Framed Structures.= By R.H.

Bow. Third thousand, 16 plates, 88 pp. 8vo. (1873)

5 0

=Theory of Voussoir Arches.= By Prof. W. CAIN. Third edition, 201 pp.

18mo, boards. (_New York, 1905_)

_net_ 2 0

=New Formulæ for the Loads and Deflections= of Solid Beams and

Girders. By W. DONALDSON. Second edition, 8vo. (_1872_)

4 6

=Plate Girder Railway Bridges.= By M. FITZMAURICE. 4 plates, 104 pp.

8vo. (_1895_)

6 0

=Pocket Book of Calculations in Stresses.= By E.M. GEORGE. 66 illus.

140 pp. royal 32mo, half roan. (_1895_)

3 6

=Strains on Braced Iron Arches= and Arched Iron Bridges. By A.S.

HEAFORD. 39 pp. 8vo. (_1883_)

6 0

=Tables for Roof Framing.= By G.D. INSKIP. Second edition, 451 pp.

8vo, leather. (_New York, 1905_)

_net_ 12 6

=Stresses in Girder and Roof Frames,= for both dead and live loads,

by simple Multiplication, etc. By F.R. JOHNSON. 28 plates, 215 pp.

crown 8vo. (_1894_)

6 0

=A Graphical Method for Swing Bridges.= By B.F. LA RUE. 4 plates, 104

pp. 18mo, boards. (_New York, 1892_)

_net_ 2 0

=Notes on Cylinder Bridge Piers= and the Well System of Foundations.

By J. NEWMAN. 144 pp. 8vo. (_1893_)

6 0

=A New Method of Graphic Statics= applied in the Construction of

Wrought Iron Girders. By E. OLANDER. 16 plates, small folio. (_1887_)

10 6

=Reference Book for Statical Calculations.= By F. RUFF. With diagrams,

140 pp. crown 8vo. (_1906_)

_net_ 5 0

=The Strength and Proportion of Riveted Joints.= By B.B. STONEY. 87

pp. 8vo. (_1885_)

5 0

=The Anatomy of Bridgework.= By W.H. THORPE. 103 illus. 190 pp. crown

8vo. (_1906_)

_net_ 6 0

CEMENT AND CONCRETE.

=Portland Cement:= its Manufacture, Testing and Use. By D.B. BUTLER.

Second edition, 97 illus. 396 pp. demy 8vo. (_1905_)

_net_ 16 0

=Theory of Steel-Concrete Arches= and of Vaulted Structures. By W.

CAIN. Fourth edition, 27 illus. 212 pp. 18mo, boards. (_New York,

1906_)

_net_ 2 0

=Cement Users' and Buyers' Guide.= By CALCARE. 115 pp. 32mo, cloth.

(_1901_)

_net_ 1 6

=Diagrams for Designing Reinforced Concrete Structures.= By G.F.

DODGE. 31 illus. 104 pp. oblong folio. (_New York, 1910_)

_net_ 17 0

=Cements, Mortars, and Concretes;= their Physical properties. By M.S.

FALK. 78 illus. 176 pp. 8vo. (_New York, 1904_)

_net_ 10 6

=Concrete Construction, Methods and Cost.= By H.P. GILLETTE and C.S.

HILL. 310 illus. 690 pp. 8vo. (_New York, 1908_)

_net_ 1 1 0

=Engineers' Pocket-Book of Reinforced Concrete.= By E.L. HEIDENREICH.

164 illus. 364 pp. crown 8vo, leather, gilt edges. (_New York, 1909_)

_net_ 12 6

=Concrete Inspection.= By C.S. HILL. Illustrated, 179 pp. 12mo. (_New

York, 1909_)

_net_ 4 6

=Reinforced Concrete.= By E. MCCULLOCH. 28 illus. 128 pp. crown 8vo.

(_New York, 1908_)

_net_ 6 6

=Concrete and Reinforced Concrete.= By H.A. REID. 715 illus. 884 pp.

royal 8vo. (_New York, 1907_)

_net_ 21 0

=Theory and Design of Reinforced Concrete Arches.= By A. REUTERDAHL.

41 illus. 126 pp. 8vo. (_New York, 1908_)

_net_ 8 6

=Practical Cement Testing.= By W.P. TAYLOR. With 142 illus. 329 pp.

demy 8vo. (New York, 1906)

_net_ 12 6

=Concrete Bridges and Culverts.= By H.G. TYRRELL. 66 illus. 251 pp.

crown 8vo, leather

_net_ 12 6

CIVIL ENGINEERING.

CANALS, SURVEYING.

(_See also_ IRRIGATION _and_ WATER SUPPLY.)

=Practical Hints to Young Engineers Employed on Indian Railways.= By

A.W.C. ADDIS. With 14 illus. 154 pp. 12mo. (_1910_)

_net_ 3 6

=Levelling,= Barometric, Trigonometric and Spirit. By I.O. BAKER.

Second edition, 15 illus. 145 pp. 18mo, boards. (_New York, 1903_) ..

_net_ 2 0

=Notes on Instruments= best suited for Engineering Field Work in India

and the Colonies. By W.G. BLIGH. 65 illus. 218 pp. 8vo. (_1899_)

7 6

=The Sextant and other Reflecting Mathematical Instruments.= By

F.R. BRAINARD. 33 illus. 120 pp. 18mo, boards. (_New York, 1891_)

_net_ 2 0

=Practical Designing of Retaining Walls.= By Prof. W. CAIN. Fifth

edition, 14 illus. 172 pp. 18mo, boards. (_New York, 1908_)

_net_ 2 0

=The Maintenance of Macadamised Roads.= By T. CODRINGTON. Second

edition, 186 pp. 8vo. (_1892_)

7 6

=Retaining Walls in Theory and Practice.= By T.E. COLEMAN. 104 illus.

160 pp. crown 8vo. (_1909_)

_net_ 5 0

=The Barometrical Determination of Heights.= By F.J.B. CORDEIRO.

Crown 8vo, limp leather. (_New York, 1898_)

_net_ 4 6

=On Curved Masonry Dams.= By W.B. COVENTRY. 8vo, sewed. (_1894_)

2 0

=A Practical Method of Determining the Profile of a Masonry Dam.= By

W.B. COVENTRY. 8vo, sewed. (_1894_)

2 6

=The Stresses on Masonry Dams= (oblique sections). By W.B. COVENTRY.

8vo, sewed. (_1894_)

2 0

=Tables for facilitating the Calculation of Earthworks.= By D.

CUNNINGHAM. 120 pp. royal 8vo

10 6

=Handbook of Cost Data for Contractors and Engineers.= By H.P.

GILLETTE. 1854 pp. crown 8vo, leather, gilt edges. (_New York, 1910_)

_net_ 1 1 0

=Rock Excavation, Methods and Cost.= By H.P. GILLETTE. 56 illus. 376

pp. crown 8vo. (_New York, 1904_)

_net_ 12 6

=High Masonry Dams.= By E.S. GOULD. With illus. 88 pp. 18mo, boards.

(_New York, 1897_)

_net_ 2 0

=Grace's Tables for Curves,= with hints to young engineers. 8 figures,

43 pp. oblong 8vo. (_1908_)

_net_ 5 0

=Grace's Earthwork Tables.= 36 double-page tables, 4to. (_1907_)

_net_ 12 6

=Railway Tunnelling= in Heavy Ground. By C. GRIPPER. 3 plates, 66 pp.

royal 8vo. (_1879_)

7 6

=Levelling and its General Application.= By T. HOLLOWAY. Second

edition, 53 illus. 147 pp. 8vo. (_1895_)

5 0

=Waterways and Water Transport= in different Countries. By J.S. JEANS.

55 illus. 520 pp. 8vo. (_1890_)

_net_ 9 0

=Table of Barometrical Heights to 20,000 Feet.= By W.H. MACKESY, with

some practical suggestions by Sir Guildford Molesworth. 1 plate, 24

pp. royal 32mo. (_1882_)

3 0

=Aid Book to Engineering Enterprise.= By E. MATHESON. Third edition,

illustrated, 916 pp. medium 8vo, buckram. (_1898_)

1 4 0

=A Treatise on Surveying.= By R.E. MIDDLETON and O. CHADWICK. Second

edition, royal 8vo.

Part I. 11 plates, 296 pp. (_1904_)

10 6

" II. Fully illustrated, 334 pp. (_1906_)

10 6

=A Pocket Book of Useful Formulæ and Memoranda,= for Civil and

Mechanical Engineers. By Sir G.L. MOLESWORTH and H.B. MOLESWORTH. With

an Electrical Supplement by W.H. MOLESWORTH. Twenty-sixth edition, 760

illus. 901 pp. royal 32mo, French morocco, gilt edges. (_1908_)

_net_ 5 0

=The Pocket Books of Sir G.L. Molesworth and J.T. Hurst,= printed on

India paper and bound in one vol. Royal 32mo, russia, gilt edges.

_net_ 10 6

=Metallic Structures: Corrosion and Fouling and their Prevention.= By

J. NEWMAN. Illustrated, 385 pp. crown 8vo. (_1896_)

9 0

=Scamping Tricks and Odd Knowledge= occasionally practised upon Public

Works. By J. NEWMAN. New impression, 129 pp. crown 8vo. (_1908_)

_net_ 2 0

=Earthwork Slips and Subsidences= on Public Works. By J. NEWMAN.

240 pp. crown 8vo. (_1890_)

7 6

=Co-ordinate Geometry= as applied to Land Surveying. By W. PILKINGTON.

5 illus. 44 pp. 12mo. (_1909_)

_net_ 1 6

=Diagrams for the Graphic Calculation of Earthwork Quantities.= By

A.H. ROBERTS. Ten cards, fcap. in cloth case

_net_ 10 6

=Pioneering.= By F. SHELFORD, illustrated. 88 pp. crown 8vo. (_1909_)

_net_ 3 0

=Topographical Surveying.= By G.J. SPECHT. Second edition, 2 plates

and 28 illus. 210 pp. 18mo, boards. (_New York, 1898_)

_net_ 2 0

=Spons' Dictionary of Engineering,= Civil, Mechanical, Military and

Naval. 10,000 illus. 4300 pp. super royal 8vo. (_1874, Supplement

issued in 1881_). Complete with Supplement, in 11 divisions

_net_ 3 10 0

Ditto ditto in 4 vols.

_net_ 3 3 0

=Surveying and Levelling Instruments.= By W.F. STANLEY. Third edition,

372 illus. 562 pp. crown 8vo. (_1901_)

7 6

=Surveyor's Handbook.= By T.U. TAYLOR. 116 illus. 310 pp. crown 8vo,

leather, gilt edges. (_New York, 1908_)

_net_ 8 6

=Logarithmic Land Measurement.= By J. WALLACE. 32 pp. royal 8vo.

(_1910_)

_net_ 5 0

=Hints on Levelling Operations.= By W.H. WELLS. Second edition, 8vo,

sewed. (_1890_)

_net_ 1 0

=The Drainage of Fens and Low Lands= by Gravitation and Steam Power.

By W.H. WHEELER. 8 plates, 175 pp. 8vo. (_1888_)

12 6

=Stadia Surveying,= the theory of Stadia Measurements. By A. WINSLOW.

Fifth edition, 148 pp. 18mo, boards. (_New York, 1902_)

_net_ 2 0

=Handbook on Tacheometrical Surveying.= By C. XYDIS. 55 illus. 3

plates, 63 pp. 8vo. (_1909_)

_net_ 6 0

DICTIONARIES.

=Technological Dictionary in the English, Spanish, German and French

Languages.= By D. CARLOS HUELIN Y ARSSU. Crown 8vo.

Vol. I. ENGLISH-SPANISH-GERMAN-FRENCH.

609 pp. (_1906_)

_net_ 10 6

Vol. II. GERMAN-ENGLISH-FRENCH-SPANISH.

720 pp. (_1908_)

_net_ 10 6

Vol. III. FRENCH-GERMAN-SPANISH-ENGLISH.

In preparation.

Vol. IV. SPANISH-FRENCH-ENGLISH-GERMAN.

750 pp. (_1910_)

_net_ 10 6

=English-French and French-English Dictionary of the Motor-Car, Cycle

and Boat.= By F. LUCAS. 171 pp. crown 8vo. (_1905_)

_net_ 5 0

=Spanish-English Dictionary of Mining Terms.= By F. LUCAS. 78 pp. 8vo.

(_1905_)

_net_ 5 0

=English-Russian and Russian-English Engineering Dictionary.= By L.

MEYCLIAR. 100 pp. 16mo. (_1909_)

_net_ 2 6

=Reed's Polyglot Guide to the Marine Engine,= in English, French,

German and Norsk. Second edition, oblong 8vo. (_1900_).

_net_ 6 0

DOMESTIC ECONOMY.

=Food Adulteration and its Detection.= By J.P. BATTERSHALL. 12 plates,

328 pp. demy 8vo. (_New York, 1887_)

15 0

=How to Check Electricity Bills.= By S.W. BORDEN. 41 illus. 54 pp.

crown 8vo. (_New York, 1907_)

_net_ 2 0

=Practical Hints on Taking a House.= By H.P. BOULNOIS. 71 pp. 18mo.

(_1885_)

1 6

=The Cooking Range,= its Failings and Remedies. By F. DYE. 52 pp.

fcap. 8vo, sewed. (_1888_)

0 6

=The Kitchen Boiler and Water Pipes.= By H. GRIMSHAW. 8vo, sewed.

(_1887_)

_net_ 1 0

=Cookery and Domestic Management,= including economic and middle class

Practical Cookery. By K. MELLISH. 56 coloured plates and 441 illus.

987 pp. super-royal 8vo. (_1901_)

_net_ 16 0

=Spons' Household Manual.= 250 illus. 1043 pp. demy 8vo. (_1902_)

7 6

Ditto ditto half-bound French morocco

9 0

=Handbook of Sanitary Information= for Householders. By R.S. TRACY. 33

illus. 114 pp. 18mo. (_New York, 1900_)

2 6

DRAWING.

=The Ornamental Penman's,= Engraver's and Sign Writer's Pocket Book of

Alphabets. By B. ALEXANDER. Oblong 12mo, sewed

0 6

=The Draughtsman's Handbook= of Plan and Map Drawing. By G.G. ANDRE.

87 illus. and 34 plain and coloured plates, 162 pp. crown 4to.

(_1891_)

9 0

=Slide Valve Diagrams:= a French Method for their Construction. By L.

BANKSON. 18mo, boards. (_New York, 1892_) . . .

_net_ 2 0

=A System of Easy Lettering.= By J.H. CROMWELL. With Supplement by G.

MARTIN. Sixth thousand, oblong 8vo. (_New York, 1900_)

_net_ 2 0

=Plane Geometrical Drawing.= BY R.C. FAWDRY. Illustrated, 185 pp.

crown 8vo. (_1901_)

_net_ 3 0

=Twelve Plates on Projection Drawing.= By O. GUETH. Oblong 4to. (_New

York, 1903_)

_net_ 3 0

=Hints on Architectural Draughtsmanship.= By G.W.T. HALLATT. Fourth

edition, 80 pp. 18mo. (_1906_)

_net_ 1 6

=A First Course of Mechanical Drawing= (Tracing). By G. HALLIDAY.

Oblong 4to, sewed

2 0

=Drawings for Medium-sized Repetition Work.= By R.D. SPINNEY. With 47

illus. 130 pp. 8vo. (_1909_)

_net_ 3 6

=Mathematical Drawing Instruments.= By W.F. STANLEY. Seventh edition,

265 illus. 370 pp. crown 8vo. (_1900_)

5 0

ELECTRICAL ENGINEERING.

=Practical Electric Bell Fitting.= By F.C. ALLSOP. Tenth edition, 186

illus. including 8 folding plates, 185 pp. crown 8vo. (_1903_)

3 6

=Telephones:= their Construction and Fitting. By F.C. ALLSOP. Eighth

edition, 184 illus. 222 pp. crown 8vo. (_1909_)

3 6

=Thermo-electric Reactions= and Currents between Metals in Fused

Salts. By T. ANDREWS. 8vo, sewed. (_1896_)

1 0

=Auto-Transformer Design.= By A.H. AVERY. 25 illus. 60 pp. 8vo.

(_1909_)

_net_ 3 6

=Principles of Electric Power= (Continuous Current) for Mechanical

Engineers. By A.H. BATE. 63 illus. 204 pp. crown 8vo. (_1905_)

(FINSBURY TECHNICAL MANUAL)

_net_ 4 6

=Practical Construction of Electric Tramways.= By WILLIAM R. BOWKER.

93 illus. 119 pp. 8vo. (_1903_)

_net_ 6 0

=Design and Construction of Induction Coils.= By A.F. COLLINS. 155

illus. 272 pp. demy 8vo. (_New York, 1909_)

_net_ 12 6

=Switchboard Measuring Instruments= for Continuous and Polyphase

Currents. By J.C. CONNAN. 117 illus. 150 pp. 8vo, cloth. (_1908_)

_net_ 5 0

=Electric Cables, their Construction and Cost.= By D. COYLE and F.J.

O. HOWE. With many diagrams and 216 tables, 467 pp. crown 8vo,

leather. (_1909_)

_net_ 15 0

=Management of Electrical Machinery.= By F.B. CROCKER and S.S.

WHEELER. Eighth edition, 131 illus. 223 pp. crown 8vo. (_New York,

1909_)

_net_ 4 6

=Electric Lighting:= A Practical Exposition of the Art. By F.B.

CROCKER. Royal 8vo. (_New York._)

Vol. I. =The Generating Plant.= Sixth edition, 213 illus. 470

pp. (_1904_)

_net_ 12 6

Vol. II. =Distributing Systems and Lamps.= Second edition, 391

illus. 505 pp. (_1905_)

_net_ 12 6

=The Care and Management of Ignition Accumulators.= By H.H.U. CROSS.

12 illus. 74 pp. crown 8vo, limp. (S. & C. SERIES, NO. 19.) (_1910_)

_net_ 1 6

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=Induction Coils.= By N.H. SCHNEIDER. Second edition, 79 illus. 285

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=How to Install Electric Bells, Annunciators and Alarms.= By N.H.

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=Electricity:= its Theory, Sources and Applications. By J.T. SPRAGUE.

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=Dynamo Electric Machinery.= By Prof. S.P. THOMPSON. Seventh edition,

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HISTORICAL AND BIOGRAPHICAL.

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=Life as an Engineer:= its Lights, Shades, and Prospects. By J.W.C.

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=Pumps:= Historically, Theoretically and Practically Considered. By

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INDUSTRIAL CHEMISTRY AND MANUFACTURES.

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=Practical Treatise on the Strength of Materials.= By T. BOX. Fourth

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=Manual of the Slide Rule.= By F.A. HALSEY. Second edition, 31 illus.

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=Galvanic Circuit investigated Mathematically.= By G.S. OHM.

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=Elementary Practical Mathematics.= By M.T. ORMSBY. 420 pp. demy 8vo.

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MECHANICAL ENGINEERING.

STEAM ENGINES AND BOILERS, ETC.

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=Engineers' Sketch Book of Mechanical Movements.= By T.W. BARBER.

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=The Repair and Maintenance of Machinery.= By T.W. BARBER. 417 illus.

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=Practical Treatise on Mill Gearing.= By T. BOX. Fifth edition, 11

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=The Steam Engine considered as a Thermodynamic Machine.= By J.H.

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=Heat for Engineers.= By C.R. DARLING. 110 illus. 430 pp. 8vo.

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=Diseases of a Gasolene Automobile=, and How to Cure Them. By A.L.

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=Worm and Spiral Gearing.= By F.A. HALSEY. 13 plates, 85 pp. 18mo,

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=Commercial Efficiency of Steam Boilers.= By A. HANSSEN. Large 8vo,

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=Liquid Fuel= for Mechanical and Industrial Purposes. By E.A.

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=Elementary Text-Book on Steam Engines and Boilers.= By J.H.

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=Centrifugal Fans.= By J.H. KINEALY. 33 illus. 206 pp. fcap.

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=Mechanical Draft.= By J.H. KINEALY. 27 original tables and 13

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=The A.B.C. of the Steam Engine=, with a description of the

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=Valve Setting Record Book.= By P.A. LOW. 8vo, boards.

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=The Lay-out of Corliss Valve Gears.= By S.A. MOSS. Second

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=Steam Boilers=, their Management and Working. By J. PEATTIE.

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=Treatise on the Richards Steam Engine Indicator.= By C.T.

PORTER. Sixth edition, 3 plates and 73 diagrams, 285 pp. 8vo.

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9 0

=Practical Treatise on the Steam Engine.= By A. RIGG. Second

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=Power and its Transmission.= A Practical Handbook for the

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=Drawings for Medium Sized Repetition Work.= By R.D. SPINNEY.

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=Slide Valve Simply Explained.= By W.J. TENNANT. Revised by

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=Shaft Governors.= By W. TRINKS and C. HOOSUM. 27 illus. 97 pp.

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=Slide and Piston Valve Geared Steam Engines.= By W.H. UHLAND.

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1 16 0

=How to run Engines and Boilers.= By E.P. WATSON. Fifth

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=Position Diagram of Cylinder with Meyer Cut-off.= By W.H.

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=Practical Method of Designing Slide Valve Gearing.= By E.J.

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=Elements of Mechanics.= By T.W. WRIGHT. Eighth edition,

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METALLURGY.

IRON AND STEEL MANUFACTURE.

=Life of Railway Axles.= By T. ANDREWS. 8vo, sewed. (_1895_)

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=Microscopic Internal Flaws in Steel Rails and Propeller

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=Microscopic Internal Flaws, Inducing Fracture in Steel.= By T.

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=Relations between the Effects of Stresses= slowly applied and

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=Brassfounders' Alloys.= By J.F. BUCHANAN. Illustrated, 129 pp.

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=American Standard Specifications for Steel.= By A.L. COLBY.

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=Galvanised Iron=: its Manufacture and Uses. By J. DAVIES. 139

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=Management of Steel.= By G. EDE. Seventh edition, 216 pp.

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=Galvanising and Tinning=, with a special Chapter on Tinning

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=Cupola Furnace.= A practical treatise on the Construction and

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=Practical Notes on Pipe Founding.= By J.W. MACFARLANE. 15

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=Atlas of Designs concerning Blast Furnace Practice.= By M.A.

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=Metallography Applied to Siderurgic Products.= By H. SAVOIA.

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=Roll Turning for Sections in Steel and Iron.= By A. SPENCER.

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=French Measure and English Equivalents.= By J. BROOK. Second

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=A Dictionary of Metric and other useful Measures.= By L.

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=Rock Blasting.= By G.G. ANDRE. 12 plates and 56 illus. in

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=Winding Plants for Great Depth.= By H.C. BEHR. In two parts.

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=Practical Treatise on Hydraulic Mining in California.= By A.J.

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=Manual of Assaying Gold, Silver, Copper and Lead Ores.= By

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=Fire Assaying.= By E.W. BUSKETT. 69 illus. 105 pp. crown 8vo.

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=Miners' Geology and Prospectors' Guide.= By G.A. CORDER. 29

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=Conversations on Mines.= By W. HOPTON. Ninth edition, 33

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=Our Coal Resources= at the End of the Nineteenth Century. By

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=Hydraulic Gold Miners' Manual.= By T.S.G. KIRKPATRICK. Second

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=Economic Mining.= By C.G.W. LOCK. 175 illus. 680 pp. 8vo.

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=Mining and Ore-Dressing Machinery.= By C.G.W. LOCK. 639

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=Tests for Ores, Minerals and Metals of Commercial Value.= By

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=Practical Handbook for the Working Miner and Prospector=, and

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7 6

=Theory and Practice of Centrifugal Ventilating Machines.= By

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=Examples of Coal Mining Plant.= By J. POVEY-HARPER. Second

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=Organisation of Gold Mining Business=, with Specimens of the

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=Manual of Engineering Specifications= and Contracts. By L.M.

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=Aid Book to Engineering Enterprise.= By E. MATHESON. Third

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=Office Management.= A handbook for Architects and Civil

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=Commercial Organisation of Engineering Factories.= By H.

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=The Entropy Diagram= and its Applications. By M.J. BOULVIN. 38

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=Physical Problems and their Solution.= By A. BOURGOUGNON. 224

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=Heat for Engineers.= By C.R. DARLING. 110 illus. 430 pp. 8vo.

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=The Colourist.= A method of determining colour harmony. By

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=Engineering Thermodynamics.= By C.F. HIRSCHFELD. 22 illus. 157

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=Experimental Science=: Elementary, Practical and Experimental

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=Reform in Chemical and Physical Calculations.= By C.J.T.

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=Introduction to the Study of Colour Phenomena.= By J.W.

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=Practical Laws and Data on the Condensation of Steam in Bare

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=Approximate Estimates.= By T.E. COLEMAN. Third edition, 481

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=Practical Hints to Young Engineers Employed on Indian

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=Railroad Curves and Earthwork.= By C.F. ALLEN. Third edition,

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=Up-to-date Air Brake Catechism.= By R.H. BLACKALL.

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=Simple and Automatic Vacuum Brakes.= By C. BRIGGS, G.N.R. 11

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=Locomotive Breakdowns=, Emergencies and their Remedies. By

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=Setting out of Tube Railways.= By G.M. HALDEN. 9 plates, 46

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=Railway Engineering, Mechanical and Electrical.= By J.W.C.

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=The Construction of the Modern Locomotive.= By G. HUGHES. 300

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=Practical Hints for Light Railways= at Home and Abroad. By

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=Handbook on Railway Stores Management.= By W.O. KEMPTHORNE.

268 pp. demy 8vo. (_1907_)

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=Railroad Location Surveys and Estimates.= By F. LAVIS. 68

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=Bridge and Tunnel Centres.= By J.B. MCMASTERS. Illustrated,

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=Pioneering.= By F. SHELFORD. Illustrated, 88 pp. crown 8vo.

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=Handbook on Railway Surveying= for Students and Junior

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=Spiral Tables.= By J.G. SULLIVAN. 47 pp. 12mo, leather. (_New

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=Modern British Locomotives.= By A.T. TAYLOR. 100 diagrams of

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=Locomotive Slide Valve Setting.= By C.E. TULLY. Illustrated,

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=Sewers and Drains for Populous Districts.= By J.W. ADAMS.

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=Public Abattoirs=, their Planning, Design and Equipment. By

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JUST OUT THE LATEST

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* * * * *

Transcriber's Notes

Obvious punctuation and spelling errors and inconsistent hyphenation

have been corrected.

Italic text is denoted by _underscores_ and bold text by =equal signs=.

The OE ligature has been replaced by the separate characters.

The fractions ¼, ½ and ¾ are represented using the Latin-1 characters,

but other fractions use the / and - symbols, e.g. 3/8 or 2-5/8.

The exponents 2 and 3 are represented using ² and ³ respectively, but

other exponents are indicated by the caret character, for example,

v^{1·85}

Subscripts are simply enclosed in braces, e.g. W{0}.

Other symbols that cannot be represented have been replaced by words

in braces: {alpha}, {pi}, {therefore}, {square root} and

{proportional to}.

The skin friction formulæ given on pages 11 and 128 have been corrected

by comparison with other sources. Respectively, the formulæ were

originally printed as

_f_ = 0·00000778_l_^{9·3}_v_^{1·85}

and

_f_ = 0·00000778_l_ - ^{00·7}_v_^{1·85}

In ambiguous cases, the text has been left as it appears in the

original book.

The Theory and Practice of Model Aeroplaning · 第 12 / 12 章