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actions obtainable by stimulation of the abdominal sympathetic are not associated with sensation. The distinct reflex contraction of the abdominal muscles resulting from stimulation of the abdominal sympathetic is another reaction which it is difficult to believe is not associated with sensation. The latter phenomenon has a two-fold interest. In the first place, it is the basis of a well-known clinical symptom, the rigid belly wall, and, secondly, it represents a form of tonic contraction not directly inducible by artificial stimuli.

On examining critically Haller's, and to a less extent Lennander's paper, we are struck by the fact that the stimuli used are unnatural in character. It is not likely that the viscera are equally responsive to all forms of mechanical stimuli. Twisting, stretching, or squeezing the wall of the intestine from the outside may be ineffective, because the nerve endings in these organs are adjusted for stimuli of another kind. In the case of the bile duct and of the ureters a twist produces no vaso-motor effect, but distension by injection produces a well-marked rise of blood pressure.

The referred visceral pain was discussed next. Dr. J. Mackenzie denies that a viscus is ever directly painful, the pain felt being essentially a "referred one." For example, in pleurisy the lungs and parietal pleura are insensitive. While agreeing with Lennander in the view that the subserous layer of the pleura is sensitive, Mackenzie holds that the pain of pleurisy is mainly a referred pain due to cramp of the muscles of the thoracic wall. Mackenzie gives the following theory as to the mechanism of the different forms of "referred pain." He holds that stimulation of afferent visceral nerves by some influence increases the excitability of afferent centres in the cord connected with corresponding areas of skin. The pain is consequently referred to these cutaneous areas, and is only indirectly the result of stimulation of deep visceral

afferents.

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Head gives a somewhat different explanation. Impressed by the fact that inflammation of spinal ganglia produces herpes zoster, he was led to believe that afferent visceral fibres in their passage through the same ganglia as certain afferent cutaneous nerves can affect the adjoining cells connected with the latter and thus produce ' referred cutaneous pain." This view is opposed to Müller's law, and was finally given up by Head. He ultimately transferred the seat of the nervous mechanism from the ganglia to deeper centres in the cord. The segments of the cord connected with "referred pain " do not correspond with the segments of the spinal axis as indicated by the ganglia. Head suggests that the "referred pain areas correspond with the primitive phylogenetic segments of the cord. He leaves the mechanism of overflow unexplained. A remarkable fact is that the area of skin affected by referred pain is a mere patch or couple of patches, not a segment, but nevertheless more or less segmentally arranged.

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The deep visceral afferents from the heart are not only those which have been most fully investigated experimentally, but also form an intermediate group between the pure visceral deep afferents and those of somatic or muscular origin. The chief afferent nerve of the heart is the depressor, and the receptive field for its stimulation is its nerve terminations in the wall of the aorta. The most adequate stimulus is distension of the walls of that vessel. The result of stimulation is a lowering of blood pressure due to a diminution of vascular tone. The nature of this tone, like that of voluntary muscles, is still obscure. It is doubtful whether stimulation of the depressor gives rise to pain directly. The areas of "referred pain" given by Mackenzie are not cranial, as we should expect, since the vagus is a cranial nerve, but mainly lie in the chest wall. Tender spots, however, are also found on the head.

Prof. Sherrington then gave a brief survey of deep nonvisceral or muscular afferents. Since the work on this subject is largely due to himself, and since he has elsewhere stated his views more fully, it would not serve any good purpose to try to epitomise this part of his paper.

The paper was followed by an interesting discussion, in which Prof. J. S. Macdonald, Dr. Graham Brown, and others took part. The discussion chiefly referred to the nature and functions of the terminations of the deep

afferent muscular nerves. A number of other papers of anatomical and physiological interest were also read by the following:-Prof. Dixon (Dublin), the development of the achondroplasic skeleton; Prof. Anderson (Galway); Dr. Dickey (Belfast), the cervical pleura; Dr. Johnston (Dublin), the intercostal nerves; Drs. Goodall and Earle (London), the structure of the pancreas in relation to its functions; Dr. Maclean (Liverpool), phosphatides in the light of modern research; Prof. B. Moore (Liverpool), the chemistry of hæmolysis; Dr. S. Spicer, some points. in the mechanics of respiration; Prof. Thompson, the development of the foetal heart; Dr. Leonard Hill, F.R.S., the influence of inhalations of oxygen on the onset of muscular exhaustion; Dr. Rutherford, some points in connection with the anatomy of the cranium of the fish; Dr. Waterston, some instruments used in anthropometry.

RECENT IMPROVEMENTS IN THE INTERNALCOMBUSTION ENGINE.1

II.

WE have already explained how important in the economical development of the internal-combustion engine is an accurate and precise knowledge of the physical. properties of the working medium. The two chief features of which a knowledge is required are the calorific value' of the explosive mixture and the relation between the The specific heat and temperature of the ignited gases. calorific value has been carefully ascertained for most of the gases commonly used, but the specific-heat relation is still a matter of unfortunate uncertainty. At the Leicester meeting of the British Association in 1907, under the sectional presidency of Prof. Silvanus P. Thompson, the desirability of clearing up the doubts that surrounded this subject was so keenly felt that an important committee was appointed for "the investigation of gaseous explosions, with special reference to temperature.' An account of the findings of this committee was published in NATURE of June 24 last. From our present point of view the important result of the committee's work is expressed in the following extract from its report :-" Recent researches on the properties of the gases at high temperatures have definitely shown that the assumption of constant specific heat is erroneous, and have given sufficient information about the magnitude of the error to show that it is of material importance. The closer approximation to the real cycle which is made by taking account of the actual properties of the working fluid, though it leads to some complication of formulæ, gives compensating advantages of real practical value." This bears out, also, a remark made by the late Prof. Zeuner to the effect that "atany rate there must be dropped from the theory of the internal-combustion motors the former assumption of the constancy of the specific heats of the products of combustion. A curve connecting the specific heat at constant volume (Cv) of the mixture of gases, formed by the explosion of one part of coal gas in nine parts of air, with temperature centigrade (0), which was considered to be accurate within 5 per cent., was included in the committee's report. A formula which fits this curve closely is

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and although the constant in the second term on the righthand side of this equation can only be looked upon as a first estimate, however carefully chosen, the equation does, probably, represent the high-water mark in our present-day knowledge, and from it can be deduced the limiting theoretical efficiency of engine cycles in which such a working medium is employed.

It is well known that on the basis of a constant specific heat the ideal efficiency (n) can be found from the following equation,

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whether the cycle followed is (1) the constant-volume cycle, (2) the constant-pressure cycle, or (3) the constant-temperature cycle, an important discovery attributed to Profs. Unwin and Callendar. The problem now arises to recalculate the thermal efficiency (n) for a working medium of which the specific heat is not constant. Most of the important internal-combustion engines operate on the constant-volume cycle, and if we re-calculate the equation to suit this case, making the necessary approximations to secure a workable result of sufficient accuracy, and using the above linear law based on the British Association Committee's figures for specific heats, we find that the new efficiency equals

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4000 (1-7.

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where T2 is the maximum absolute temperature (centigrade) in the cycle, T, the suction temperature, whilst n is the value obtained from the equation

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using here the value of corresponding to the absolute zero of temperature. The value of T, is practically independent of the compression, and in round figures suitable to this calculation may be written down as 400. The value of T, for a given richness of mixture will depend upon the degree of compression before ignition, and can be calculated therefrom. In this way a new expression for the real thermal efficiency can be obtained in terms, not of T,, but of r, and the following table shows a few comparative figures worked out in this way. The figures for the air-standard efficiency are also given by way of comparison.

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It will be seen that in each case the real efficiency is about a quarter less than the "air-standard" efficiency.

This discrepancy sufficiently explains why those associated with the design and building of gas engines have expressed their dissatisfaction with the "air standard" of efficiency. The adoption of the "air standard " has led to the setting up as an ideal, to be aimed at and striven after, of a series of figures which it now appears are about one-third above the thermal efficiencies theoretically possible, and it is not surprising that engine builders, who from their practical work realised that there must be something wrong with the theory as then put forward, should have objected. It is not too much to say that had the engine builders to depend in the past solely on scientific guidance as the mainspring of their investigations, there would have been far less progress made than has been effected by the system of trial and error. Even now the state of knowledge as to gaseous specific heats is so uncertain that no accurate quantitative theory of the thermodynamics of the internal-combustion engine can be laid down. The writer has, however, endeavoured to show here and elsewhere how the problem may be investigated symbolically, and so prepared for expression in numerical form as soon as the thermal properties of the gases are actually known. Mr. Dugald Clerk, in his 1907 paper1 before the Institution of Civil Engineers, made some estimates of real efficiencies based on theoretical maximum temperatures of 1600° C. and 1000° C., and his results are given below.

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1 Proc. I.C.E, vol. clxix., p. 145.

the real maximum temperatures were also 1600° C. and 1000° C. This, however, would be open to several objections. As an instance, take the case of an engine which by improved design was made capable of giving for the same mixture and the same compression ratio a higher maximum temperature and pressure. Such an effect might be produced, let us say, by decreasing the ratio of cooling surface to volume through an alteration in the amount of pocketing. This new engine, on the basis of comparison with an ideal cycle having an identical maximum temperature, would probably show little, if any, improvement in relative efficiency over the old engine. Such a result would tend to defeat the purpose for which comparisons with ideal cycles are made. It would seem to the author that the better way would be to compare both old and new engines with an ideal cycle having a maximum temperature corresponding to the known richness of the mixture, its calorific value, and the ratio of compression.

A factor that has affected most advantageously the recent progress of the internal-combustion engine is the great improvement that has taken place in engine indicators. The old moving lever design, although thoroughly serviceable for most steam engines and for many slow-moving internal-combustion engines, has been found entirely untrustworthy with modern highspeed internal-combustion engines. A new form of instrument has been devised in which the recording lever is a beam of light, which, having no inertia, has no time-lag. This vitally important improvement in the indicators was due, in the first instance, to the prescience of Prof. Perry,1 and in its later stages to the experimental skill of Profs. Callendar and Hopkinson. The writer has recently calculated out the case of an indicator of which the free periodic time of oscillation was 1/300 sec., and has shown that explosions occurring even in so short a time as 1/200 sec. could be adequately followed and recorded. We believe that this oscillation period represents about the sensitiveness of one of the reflecting indicators used by Prof. Hopkinson at Cambridge, and the calculation serves to show how accurately the new instruments can be made to follow extremely rapid explosions.

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It would be useless to base any deductions on the records given by one of the old type of instruments in such a sharp explosion as this. Errors of as much cent. 5 per are now known to have occurred in the measurements of horse-power made by the old instruments. On the other hand, it cannot be denied that the older type was a great deal easier to handle, and that it could be used by comparatively untrained persons. The new reflecting kind, despite its accuracy of measurement to within 1 per cent. of the power, is rarely seen in workshops, and the of "indicated horsepower" has been very commonly abandoned in favour of the measurement of "brake horse-power both in the case of large and small engines. In the case of the numerous small high-speed petrol engines, the practice of actually measuring brake horse-power is often replaced by the use of a rating formula giving a "nominal" horsepower. It seems at first sight extraordinary that there should be a reversion to the old unscientific "N.H.P.. but, despite their apparent similarity, the "N.H.P." of the old days of the steam engine and boiler, and the rating H.P." of the modern petrol engine, are really based on very different considerations, and, as there appears to be every likelihood that the latter will be constantly revised with the aid of the best scientific advice possible, there is little real foundation for any scientific objection to it. The pioneer work done by Prof. Callendar in promoting this advance cannot be too gratefully acknowledged. Others have also worked at the problem since, and a considerable output of rating formulæ has resulted. D2. N That in most common use is H.P.: where D is 2.5 cylinder diameter in inches and N is the number of cylinders. This formula was put forward with the authority of the Royal Automobile Club, and experience has shown that in the great majority of cases it gives wonderfully good results. It may even doubted whether any of the far more complicated 1 "The Steam Engine," by Prof. Perry, p. 117.

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formulæ since brought forward give a more measurement. It is, of course, not fitted for use with racing motors, in which everything in design is sacrificed to piston speed, high mean pressure, and a sufficient endurance to last through a few races. For an engine having 4-inch cylinders the Royal Automobile Club formula gives a rating of 25.6 horse-power, which is about the brake horse-power that a normal engine of this size would yield when driven at a normal speed. Racing motors of this size have, however, given almost, if not quite, 100 horse-power, and even if it were possible to do so it is a question whether it is worth while to search out a formula which would embrace such divergent practice and conditions of operation. The Roval Automobile Club formula corresponds to combining a piston speed of 1000 feet per sec. with a mean pressure of 67.2 lb. per square inch. Before it can be revised a complete series of careful experiments on engines of sizes ranging from 2 inches to 10 inches should be carried out.

In the succeeding article the writer proposes to discuss details of the recent mechanical improvement of the internal-combustion engine in relation to the theoretical investigations already discussed.

H. E. WIMPERIS.

CONFERENCE OF ENGINEERS AND SHIPBUILDERS AT GLASGOW.

A JOINT summer meeting of the members of the Institution of Engineers and Shipbuilders in Scotland and of the North-east Coast Institution of Engineers and Shipbuilders was held in Glasgow on August 4, 5, and 6. It is of interest to note that, although a large number of works and shipbuilding yards was thrown open to visitors, no works in which Admiralty work is under construction were included. This arises from the firms concerned paying respect to the wishes of the Admiralty that as much secrecy as possible should be observed regarding the details and progress of Government work. Wednesday and Thursday mornings were reserved for the reading and discussion of papers, of which we give brief extracts.

Sir Andrew Noble contributed some notes on the history of propellants. Perhaps the easiest way of showing the striking difference between the old gunpowders and some of the modern propellants is to quote two tables given by the author. As both the units of heat and the quantity of gas vary considerably, depending on the pressure under which the propellant is exploded, the author has taken the transformation approximately at the pressures at which the propellants are generally used in guns.

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Cordi'e, J'alian M.D. Norwe- Nitro- NorweMark I. ballistite cordite gian 167 cellulose gian 165 Volumes of gas 875'5 810'5 913'5 899 9 934'0 909'9 Units of heat 1246'0 1305'0 1030'0 1005 5 924'0 935'5 Comparative energy 1,090,873 1,057,703 940,905 904,850 863,016 851,212 It will be seen from the tables that the comparative energies of the modern explosives are more than four times as great as those of the older propellants.

As regards the serious question of erosion, in the case of very large guns it is important to remember that,

The author has tested the capacity for erosion of several explosives, and has found these to vary considerably, but all give similar results with varied charges. Thus the erosion due to one three-quarter charge was less than that of a full charge, but two three-quarter charges gave more erosion than one full charge. Two half charges gave less, but three half charges gave more, erosion than one full charge. These experiments controvert the statement which has been made frequently that the erosion due to four three-quarter charges, as also that due to sixteen half charges, are equivalent to the erosion due to one fuli charge.

A paper on the trials and performances of the S.S. Otaki, by Engineer-Commander W. McK. Wisnom, R.N., is of interest in view of this vessel being the first merchant vessel fitted with a combination of reciprocating and turbine machinery. The Otaki was built by Messrs. Denny, of Dumbarton, and delivered in November, 1908. She has since completed a voyage to New Zealand and back, and is virtually a sister ship to the twin-screw vessels Orari and Opawa, fitted with reciprocating engines and constructed by the same builders. All three vessels belong to the New Zealand Shipping Company.

The only important differences in the vessels consist in an increase in length of the Otaki of 4 feet 6 inches to make up for the loss in cargo capacity due to three shaft tunnels instead of two, and also the modified design of the stern and stern post in the same ship. The boiler installations in the three vessels are identical. The engines of the Otaki consist of two sets of ordinary tripleexpansion reciprocating engines driving wing propellers, and a low-pressure turbine driving a central propeller. In ordinary ahead working the reciprocating engines exhaust into the turbine, and change valves are fitted so that the reciprocating engines can also exhaust direct to the condensers.

At the trials on the measured mile at Skelmorlie the Orari attained a mean speed of 14.6 knots; the Otaki, under the same conditions, attained a mean speed of more than 15 knots for a total water consumption per hour of 6 per cent. less than that of the Orari. The total water consumption per hour in the Otaki at 14.6 knots was 17 per cent. less than in the Orari at the same speed. On the run from the Clyde to Liverpool, with the vessel partly loaded, on November 21 and 22, 1908, at about half power, the coal consumption was about 1.387 lb. per horse-power per hour for all purposes. Scotch coal was used, having a heating value of about 7500 centigrade units.

As regards the performance of the Otaki on service, the coal consumption on the voyage from Liverpool to Teneriffe was II per cent. less than the mean for the sister vessels Orari and Opawa under similar conditions and at practically the same speed. For the round voyage, at the same speed, the coal consumption of the Otaki is about 8 per cent. less than that of her sister ships. The engines of the Otaki made a non-stop run from Teneriffe to New Zealand, a distance of 11,669 miles as logged, which is probably the longest continuous run yet made by marine turbine. The turbine worked perfectly satisfactorily throughout the whole round voyage.

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The New Zealand Shipping Company is to be congratulated in allowing this experiment to be made, and also for its courtesy in rendering available the very full information contained in the paper regarding the performances of their vessels.

PAPERS ON REPTILES AND FISHES.

the Miocene of Maryland is described by Mr. W. Palmer in No. 1669 of the Proceedings of the U.S. National Museum under the name of Psephophorus calvertensis, this being the first representative of the genus, which was previously known from the Tertiaries of Europe and Egypt, hitherto recorded from American deposits. It is, however, pointed out that certain dermal armour from the Zeuglodont Limestone of North America, figured by Müller in his work on Zeuglodon, probably belongs to the same genus.

while the surface of the bore subject to the more violent A NEW species of leathery, or leather-back, turtle from erosion increases approximately as the calibre or a little more, the charge of the propellant required to give to similar projectiles the same maximum velocity increases as the cube of the calibre. Consequently, unless special arrangements as to the projectile are made, or other means adopted, the life of the largest guns before re-lining must be short when compared with that of smaller guns. Attention should be given to the best method of reducing erosion when very large charges are used, either by lowering the temperature of explosion or possibly by introducing some cooling agent with the charge.

In No. 1681 of the same publication Dr. L. Stejneger gives the name Mesopeltis longifrenis to a snake from

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The first part of the second volume of the Memoirs of the Indian Museum is devoted to the initial portion of a report, by Dr. N. Annandale, on the fishes taken by the Bengal fisheries steamer Golden Crown; this section, which is illustrated with five plates, dealing with the skates, rays, and sawfishes. In the group of sting-rays and butterflyrays, new species of the genera Trygon and Urogymnus are described and named, while in the torpedo-rays, in addition to a new species of Narcine, Dr. Annandale proposes the unclassical term "Bengalichthys for a ray distinguished from Astrape by its thickened and fleshy disc, rudimentary pectoral fins, and degenerate eyes.

A second new genus of rays, Dactylobatus, has recently been proposed by Messrs. B. A. Bean and A. C. Weed in No. 1682 of the Proceedings of the U.S. National Museum for a species of which two examples were taken off South Carolina nearly a quarter of a century ago. The generic name refers to the presence of a finger-like process jutting from the middle of each pectoral fin, which, together with the subcircular form of the disc, distinguishes this handsomely spotted species from the typical rays of the genus Raia.

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In No. 1677 of the publication last quoted Messrs. D. S. Jordan and J. O. Snyder describe, under the name of Coregonus oregonius, a new "white-fish from the McKenzie River, Oregon, where it is locally known as the chisel-mouth Jack.' It is an active, predaceous fish about 18 inches in length, which takes the fly readily.

To the June number of the Zoologist Mr. R. Elmhirst, superintendent of the Marine Biological Station at Millport, communicates a note on whelks as cod-food. Cod, it is well known, feed chiefly on crustaceans, but two cases are on record where large numbers of whelks were taken from the stomachs of these fishes. Now, although these molluscs, generally with the operculums cut off, are frequently used as bait in cod-fishing, the number of whelks with their operculums in the two instances mentioned indicates that these had not been taken on lines, but devoured in the course of natural feeding. The author is of opinion that cod seize whelks when the foot is protruded, and swallow this part alone, rejecting the shell and its contents by means of a vigorous shake.

In the same issue Mr. L. E. Adams gives some additional notes on the flying-fish problem, in the course of which it is suggested that the discrepancy between the accounts of different observers with regard to the occurrence of wing-vibration may be due to the personal equation" in the matter of vision-power.

PRIMITIVE DIPROTODONTS.

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AT last, it seems, the true position of Plagiaulax, of the Dorsetshire Purbeck, described by Hugh Falconer in 1857, has been more or less definitely determined, and this by means of its early Tertiary American relative Ptilodus, of which remains, in a much more satisfactory condition than any hitherto known, have recently been discovered in Montana. These are described by Mr. J. W. Gidley in No. 1689 (vol. xxxvi., pp. 611-26) of the U.S. National Museum Proceedings under the name of P. gracilis. Of late years Plagiaulax and Ptilodus, together with a number of more or less nearly allied types, collectively forming the Multituberculata or Allotheria, have been tentatively associated with the Metatheria on account of a presumed resemblance of their cheek-teeth to those of the platypus. A study of the skull, pelvis, and limb-bones of the American genus has, however, convinced Mr. G'a'ey that this is wrong, and that the Plagiaulacidæ (together with the other Multituberculata) are really marsupials. The unequal development of the fore and hind limbs, the characters of the incisors, the form of the palate, and the position of the cheek-teeth indicate, in his opinion, a close, although not ancestral, relationship with the diprotodont marsupials.

of Fossil Mammalia in the British Museum ") endorsed, in a somewhat modified manner, this opinion, regarding the Multituberculata as primitive diprotodonts presenting some very specialised features. In the course of his investigation Mr. Gidley has been led to conclude that Bolodon of the English Purbeck is inseparable from Plagiaulax, while the American Chirox is identical with Ptilodus.

The dental formula of Ptilodus is i., c.ỗ, p.ĝ, m.i The lower jaw is attached obliquely to the skull in such a manner that its condyle is raised above the line of the cheek-teeth (thereby doing away with an objection raised by Owen against the herbivorous nature of Plagiaulax), and the greater portion of the large cutting lower premolar does not, in consequence, bite against the upper cheek-teeth, which extend considerably in advance of the Mr. Gidley's views, especially if the Triassic Microlestes (a name which it has recently been proposed to replace by Thomasia) belong to the same group as Plagiaulax, will considerably modify opinion with regard to the origin and radiation of the diprotodonts.

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PROBLEMS OF AVIATION.

THE interim report of the Advisory Committee for Aeronautics, which, in his recent speech in the House of Commons, Mr. Haldane promised shortly, has now been published (Cd. 4711). It will be remembered that the duty of the committee is to advise on questions submitted to it by the Government departments to which the work of constructing and experimenting with aeroplanes and dirigibles has been entrusted. This work necessitates, in some cases, experimental research at the National Physical Laboratory. The committee is intended generally to advance the applications of the science of aeronautics by such means as may seem best. It has arranged already for a series of reports as to the present state of knowledge on the questions which will have to be considered. These reports are to include papers on the following subjects:-Mr. A. Mallock, on general questions to be studied; Dr. T. E. Stanton, on recent researches on the forces on plane surfaces in a uniform current of air; Sir G. Greenhill, on stability and on the screw propeller; Dr. W. N. Shaw, on wind structure, dealing especially with the phenomena of gusts, and on the variation of wind velocity with height; Mr. F. W. Lanchester, on petrol motors for aëronautical purposes; Dr. W. Rosenhain, on light alloys; and the secretary (Mr. F. J. Selby), on existing knowledge on the subject of the accumulation of electrostatic charges on balloons, and the precautions to be adopted to avoid the dangers arising therefrom.

To make it possible to decide what work should be undertaken first at the National Physical Laboratory, the committee drew up a list of desirable experiments as follows:

I.-General Questions in Aërodynamics.

(1) Determination of the vertical and horizontal components of the force on inclined planes in a horizontal current of air, especially for small angles of inclination to the current.

(2) Determination of surface friction on plates exposed to a current of air.

(3) Centre of pressure for inclined planes.

(4) Distribution of pressure on inclined planes. (5) Pressure components, distribution of pressure and centre of pressure for curved surfaces of various forms. (6) Resistance to motion of bodies of different shapes ; long and short cylinders, &c.

(7) Combinations of planes; effect on pressure components of various arrangements of two or more planes.

II. Questions Especially Relating to Aëroplanes. (8) Resistance components for aeroplane models. (9) Resistance of struts and connections. (10) Resistance of different stabilising planes, both horizontal and vertical.

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This is practically a confirmation of the original view (11) Problems connected with stability :-(.)
of Falconer, who regarded Plagiaulax as related to Hypsi-matical investigation of stability; (ii) the stability of aero
Prymnodon (Potorus). Cope (who was followed by Mr. curves of different section and of different plan (Turnbull's
Lydekker on p. 195 of the fifth volume of the " Catalogue experiments); (iii.) effect of stabilising planes and investiga-

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(22) Production of hydrogen. (23) Gas-tightness of fabrics.

(24) Detection of leakage.

(25) Air resistance to ships of different form; experiments on models :-(i.) effect of shape of ends; (ii.) effect

of length; (iii.) variation with speed; (iv.) distribution of pressure as affecting stability, strength in construction, position of propellers, fins, &c.; (v.) total resistance of models rigged to represent different balloons.

(26) Questions as to stability of airships in different positions.

(27) Stabilising and steering appliances, fins, rudders, &c.; form and position.

(28) General design.

(29) Navigation of airships. Mooring, &c.

(30) Efficiency and position of propellers for airships. (31) Motors for airship work.

VI.-Meteorology.

(32) General information relating to variations of wind velocity and phenomena connected with gusts of wind. (33) Relative variation in speed and direction of the wind at different heights above the earth's surface. (34) Vertical movements in the air.

(35) Rotary movements in the air. (36) Electrical phenomena.

(37) Formation of clouds, snow, hail, &c. Eventually the committee decided that the following researches should be undertaken at once:

(a) Experiments on air resistance and on air friction as outlined in (1) to (7) above, and including experiments on models of airships and aëroplanes, resistances of wires and connecting stays, &c.

(b) Motor tests.

(c) Propeller experiments.

(d) Tests for gas-tightness of materials suitable for dirigibles.

(e) Experiments on the behaviour of different materials with reference to the accumulation of electrostatic charge, and generally as to means of protecting airships from the effect of electrical discharges.

The interim report points out that additions to the existing buildings at the National Physical Laboratory have been found necessary to provide space for part of the experimental work, while a special building is also being provided for the whirling table referred to below. The equipment which is now being installed comprises the following:-

(i.) A wind channel 4 feet square and about 20 feet long, with a fan giving a draught of 40 feet per second, special arrangements being made to obtain a uniform flow. This will be employed for the determination of the air-pressure components on plane and curved surfaces, for the resistance of models of airships and aeroplanes, and for observations on the centre of pressure, frictional resistance, stability, &c.

(ii.) A whirling table of about 70 feet diameter. For this a special building is being erected; the table itself is under construction in the laboratory. It will be employed for a repetition of Dines's and Langley's experiments, as well as for propeller tests, which are urgently called for.

(iii.) Two wind towers for experiments in the open. These will enable some of the air-channel experiments to be repeated on a larger scale in the natural wind, and will, it is hoped, afford valuable information as to the varying conditions which obtain in practice.

(iv.) Apparatus for efficiency tests on high-speed motors up to 50 horse-power.

In addition, certain machine tools, &c., are being provided for workshop use.

The evidences provided by the interim report of the activity of the committee are gratifying in view of the activity being displayed in other countries in practical aviation. We notice that, on August 7, M. Sommer added another triumph to France in this province of aëronautics. M. Sommer beat the world's record for length of time in the air by flying at Châlons for 2h. 27m. 15s. The record was previously that of Mr. Wilbur Wright, who, on December 31 last, remained in the air at Le Mans for 2h. 20m. 238.

THE MAGNETIC OBSERVATORIES OF THE U.S. COAST AND GEODETIC SURVEY.1

A LIBERAL addition made in 1899 to the funds available for magnetic work by the U.S. Coast and Geodetic Survey enabled a great extension to be made in the direction of magnetic observatories. Previously to that date the only magnetographs run by the Survey were an old Brooke instrument, first set up in 1860 at Key West, and an Adie instrument installed in 1882 at Los Angeles, and subsequently in use elsewhere. These two instruments are still in use, the Brooke in modified form at Vieques, the Adie at Cheltenham (fourteen miles south-east of Washington, D.C.), the central station of the Survey. Cheltenham also possesses a new set of Eschenhagen instruments, and similar instruments were also obtained for Baldwin, Sitka, and Honolulu. The curves from the five observatories are tabulated at a central office, and the volumes containing the earliest years' results have recently appeared. The material is dealt with after a uniform plan. Each volume discusses the buildings and instruments, and enumerates the base-line and scale-value changes. It is interesting to learn that the experience at Cheltenham is decidedly favourable to the old Adie type, on account of its greater stability and the less frequent adjustments required." Another instrumental point of interest relates to the temperature coefficients of the horizontal force instruments. That of the Adie instrument appears exceptionally large for an instrument of its type, but it is less than half the average value for the four Eschenhagen instruments, and only one of the latter is worse than the Brooke in this respect. When a rise of 1° C. in temperature produces the same effect in the trace as a fall of 177 in the force-as seems to be the case at Honolulu-satisfactory elimination of temperature effects must be troublesome. If the cause lies in the quartz-fibre suspension, a substitute should be sought for.

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The greater part of each volume is devoted to the hourly readings from the curves. Declination and horizontal intensity results are given for all the stations, but vertical intensity results only for Cheltenham. Mean hourly values are deduced for each month, first from all the days, and, secondly, from the ten least disturbed days. The latter form the basis of the regular diurnal inequalities given for each month. Inequalities are calculated for the northerly and easterly components as well as for declination and horizontal intensity, and at Cheltenham for dip as well as for vertical intensity. Under the heading Daily Range of Declination" we have tables of values 1 Results of Observations made at the Coast and Geodetic Survey Magnetic Observatories, Cheltenham. Maryland, 1901-4. pp. 206; Baldwin, Kansas, 1901-4, pp. 138; Sitka, Alaska, 1902-4, pp. 129; near Honolulu, Hawaii, 1902-4. rp. 130; and Vieques, Porto Rico. 1903-4, pp. 70. By Daniel L. Hazard, Computer, Division of Terrestrial Magnetism. (Washington: Government Printing Office, 1909.)

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