WIND STRESSES [FLEMING] Six Jyfono&ra pAr on ~./- , v' / Wind WIND PRESSURE FACTORS SPECIFICATION REQUIREMENTS MILL-BUILDING STRESSES RIGID JOINT WIND BRACING FOR OFFICE BUILDINGS BY ROBINS FLEMING Engineer, American Bridge Company , New York REVISED AND ENLARGED REPRINTS FROM ENGINEERING NEWS ENGINEERING NEWS HILL BUILDING, NEW YORK 1915 Copyright, 1915, by Hill Publishing Co. PREFACE Wind is everywhere. It affects all structures. Every engineer, or even every person who ever sees an engineer, has a personal interest in the effect of wind on structures. That is the subject of the present book. Ignorance is not always bliss. If it be true as seems very likely that wind is preeminently a matter concern- ing which no one knows he knows not, then this book deserves to have many readers. There is a fresh touch to what the author says. His main argument throughout is common sense. In this respect his frame of mind is catching; the reader will find himself saner and sounder for having read the book. When the author refers to intricate studies of wind action, claimed to show the need for radical changes in building practice, he leads us to notice the practical fact that these intricate studies are based on tests made in mild breezes, and can hardly be safe guides as to what happens in storms. Six articles which appeared in ENGINEERING NEWS, most of them in the early months of 1915, make up this book. One of the six, however No. 6 is so changed from the form in which it was printed March 13, 1913, that it is new. And this subject, the stress calculation for tier-building frames without diagonals, is so far without any literature. The many slow hours of work which the author con- sumed in searching out and studying the material re- quired for writing this book merit the reader's apprecia- tion. EDITOE Engineering News. 382055 CONTENTS Page I Wind Pressure Formulas and Their Experi- mental Basis II Wind Stresses in Steel Mill Buildings . . 13 III Wind Stresses in Eailroad Bridges ^7 IV Wind Stresses in Highway Bridges . . . V Windbracing Kequirements in Municipal Building Codes 53 VI Windbracing without Diagonals for Steel- Frame Office Buildings 61 Wind Pressure Formulas and Their Experimental Basis SYNOPSIS A discussion of the current formu- las for relation between wind pressure and velocity, relation between pressure on normal planes and planes inclined to the wind, and several other phases of wind pressure. The author brings out strikingly how inadequate is the experimental basis for the formulas and figures commonly employed. The purpose of this article is to give the basis from which some of the commonly used formulas for wind pressure are derived. Even the engineer who wishes to know only the wind pressure in pounds per square foot for which he shall make provision in his structure will be better equipped for designing if he is acquainted with the foundations on which ordinary practice rests. KELATION BETWEEN WIND PBESSUBE AND VELOCITY In view of the extent of the literature on the subject it might reasonably be supposed that the elementary prin- ciples of wind pressure are determined, at least theoretic- ally. How near this is to being the case may be inferred from the following extracts taken from two modern American textbooks, each of which is regarded as an authority. Marburg, in his Framed Structures and Girders, under ''Wind Pressure," writes: Theoretically the pressure p, in Ib. per sq.ft., on a plane surface normal to the direction of flow of a fluid having a relative velocity v, in ft. per sec., is equal to the weight of a vertical column of the fluid having a cross-section of 1 sq.ft. and a height h, in ft. equal to that through which a freely moving body must fall to acquire the velocity v. If w denotes the weight of the fluid, in Ib. per cu.ft., wv 2 p = Wh = _ (1, For air at a temperature of 32 F. and at a barometric pressure of 760 mm., w = 0.081. Letting g = 32.2, p = 0.00126 v (2) [i] If V denotes the velocity of the wind in miles per hour, v =. 1.47 V, whence equation (2) becomes p 0.0027V 2 (3) Burr and Falk, in The Design and Construction of Metallic Bridges, under "Stresses due to Wind" write: If the wind were directed as a finite stream against an infinitely large surface, so that the direction of the air is completely changed, an equation expressing the force against that surface may be obtained from the laws of mechanics. Let W == the weight of air directed against any normal surface in a given time; w = the weight in pounds of one cubic foot of air; v = the velocity of wind in feet per second; a == the area of cross-section of the wind stream, Then W = wav. Let M = the mass of air of the weight W; g = the acceleration due to gravity = 32.2 feet per second; P = the force acting on the area a, Wv wav a Then F = Mv = = (1) g g If a be taken at 1 sq.ft., and w at 0.0807 Ib. per cu.ft. for a temperature of 32 F. and a barometric pressure of 760 mm., and if v be replaced by V, the velocity in miles per hour, then P = 0.0054 V 2 (2) The reader will observe that starting with the same as- sumptions one author finds the resultant pressure to be twice that of the other. Both authors make haste to write that the theoretical conditions upon which their formula is* based do not exist. A cushion of air is formed in front of the plate and a partial vacuum at the back ; there is a certain amount of air friction and the change of direction is not complete. The student facing such conflicting theories on the very fundamentals of wind pressure may well raise the question of authority. It is almost impossible to give undue credit to Sir Isaac Newton for his work in the realms of science and mathe- matics. His great book was the Philosophia Naturalis Principia Mathematica, or "The Mathematical Principles of Natural Philosophy," commonly called the Principia. Originally published in 1686, revised editions were is- sued in 1713 and 1726. Modern hydrodynamics had its [2] origin in the second book, treating of Motion of Bodies in Resisting Mediums. Section VIII of this book is entitled ''Of Motion Propagated through Fluids." A translation of Prop. XLVIII (Newton wrote in Latin) reads: The velocities of pulses propagated in an elastic fluid are in a ratio compounded of the subduplicate ratio of the elastic force directly, and the subduplicate ratio of the density in- versely; supposing- the elastic force of the fluid to be pro- portional to its condensation. This means that the velocity v varies as -7, or p varies V a as dv 2 . For wind pressure, the density of the air being constant, we have the law that the pressure varies di- rectly as the square of the velocity, which has remained almost undisputed since Newton's day. Furthermore, according to Newton, for an area of v 2 unity, p = dh, in which h = ^ is the distance through which a heavy body must fall to acquire the velocity v, g being the coefficient of gravity or 32.2. This may be called the Newtonian theory, and has been followed by a host of writers, including Marburg (quoted above). W. J. M. Rankine was one of the master mathema- ticians of the nineteenth century. In his fifteenth year his uncle presented him with a copy of Newton's Prin- cipia, which he read carefully. He remarks, "This was the foundation of my knowledge of the higher mathe- matics, dynamics and physics." But the pupil did not blindly follow the master. In his Applied Mechanics, he has a section devoted to "Mutual Impulse of Fluids and Solids." A jet of fluid A, striking a smooth sur- face, is deflected so as to glide along the surface in that path which makes the smallest angle with its original di- rection of motion. Let v be the velocity of the particle of fluid, q the volume discharged per second equal to Av, d the density, and the angle by which the direction of motion is deflected; then is the momentum of the y quantity of fluid whose motion is deflected per second. With these notations the general equation for the force [3] Fx perpendicular to the plane in question is found to be For the particular case of the plane at right angles to the jet or B = 90, 9 9 This may be called the impact theory, and is followed in some textbooks, including that of Burr and Falk. From the time of Newton until this day a long line of investigators have sought by experiment to obtain the value of Tc in the formula P = kV 2 f in which P = pres- sure in Ib. per sq.ft. and V = velocity in miles per hour. As before noted, according to the Newton formula Ic is 0.0027 and with the same assumptions according to Ran- kine Tc is 0.0054. What is known as the Smeaton for- mula held almost universal sway for 150 years and is still in use. It is very simple, P = 1 / 200 V 2 . In the Philoso- phical Transactions of the Royal Society, England, for the year 1759 is a lengthy paper entitled, An Experi- mental Enquiry Concerning the Natural Power of Water and Wind to Turn Mills, and Other Machines, Depend- ing on a Circular Motion. By Mr. J. Smeaton, F. R. 8. Part III is "On the Construction and Effects of Wind- mill-Sails/' For his experiments Smeaton constructed an elaborate machine or whirling-table in which fixed sails revolved through the air about a given axis and their velocities were measured by the weights lifted. A foot- note reads: Some years ago Mr. Rouse, an ingenious gentleman of Hasborough in Leicestershire, set about trying experiments on the velocities of the wind, and force thereof upon plain surfaces and windmill sails. It is presumed, though not so stated, that Mr. Rouse used a whirling-table similar to that described by Smeaton. Further on in the paper a table "containing the velocity and force of wind, according to their common appellations," is found introduced with : The following table which was communicated to me by my friend Mr. Rouse, and which appears to have been con- structed with great care, from a considerable number of [4] facts and experiments, and which having relation to the sub- ject of this article; I here insert as he sent it to me; but at the same time must observe that the evidence for those num- bers where the velocity of the wind exceeds 50 miles an hour, do not seem of equal authority with those of 50 miles an hour and under. It is also to be observed, that the numbers in column 3 are calculated according to the velocity of the wind, which in moderate velocities, from what has been be- fore observed, will hold very nearly. From this introduction it is impossible to tell where ex- periment ended and theory began. The coefficient of V* according to the figures given in the third column of the table is found to be 0.00492, or V 2 oo nearly. It is hard to understand how a formula resting upon such a slender foundation should have had such wide vogue. The most careful experiments of recent years for the pressure on flat plates of moderate size normal to the di- rection of a uniform wind give a value of Tc from 0.0032 tc 0.004. Hence the formula P = 0.004 V 2 may be safely used. It is interesting to note that Weisbach, in his monumental work, the Mechanics of Engineering, followed Newton's method but multiplied the value of Tc as found by this method by a coefficient 1.86, stating that about two-thirds of the action is upon the front and about one-third upon the rear surface. He based his coefficient upon the experiments of Dubuat (about 1780) and Thi- bault (1826). The U. S. Weather Bureau uses the formula P = 0.004 ^-F 2 oO in which B = height of barometer in inches. This for the Tt engineer is an unnecessary refinement as ^ varies but oU little from unity. Wolff in his book The Windmill as a Prime Mover takes into account also the effect of tem- perature in determining wind pressure. At sea level for a wind velocity of 40 miles per hour he finds pressures of 8.6 Ib. per sq.ft. for F. to 7.08 Ib. for 100 F. For a velocity of 80 miles per hour he finds pressures of 34.98 Ib. per sq.ft. at F. to 28.86 Ib. at 100 F. WIND-PRESSURE COEFFICIENT FOR INCLINED SURFACES For the intensity of wind pressure on inclined surfaces we have a wide range of values from which to choose. [ 5 ] Tiberius Cavallo, F. E. S., etc., in 1803, published a four- volume treatise on The Elements of Natural or Experi- mental Philosophy. The writer has never seen the treatise quoted, but Chapter IV of Book II, "Of the Action of ^"onelastic Fluids in Motion," and Chapter X of the same book, "Of Air in Motion, or of the Wind," are written in a truly scientific spirit and are readable today. A proposition of Cavallo's reads, "The forces of a fluid medium on a plane cutting the direction of its motion with different inclinations successively, are as the square? of the sines of these inclinations." This, however, ia implied by the great Newton in the Principia, Book II, Prop. XXXIV. Among recent writers Spofford in "The Theory of Structures" deduces the same theoretical re- sults. As these results differ widely from those obtained by experiment, recourse must be had to empirical formulas. Among such, Button's formula has been used in England and the United States perhaps more than all others com- bined. It is still found in the latest editions of many technical books. The experiments upon which it is based were decidedly crude. Tract XXXVI of Tracts on Mathematical and Philosophical Subjects by Charles Hutton, LL.D., F.E.S., Professor of Mathematics in the Eoyal Military Academy of Woodwich, England, entitled, "Eesistance of the Air Determined by the Whirling- Machine," records his experiments. Hutton secured a whirling-machine and during 1786 and 1787 experi- mented with hemispheres and cones. Under date of July 23, 1788, he records: Prepared the machine to make experiments with figures of shapes different from the foregoing ones. Procuring a thin rectangular plate of brass to fix on the arm of the ma- chine; its weight 11^ oz. and its dimensions 8 in. by 4 in., consequently its area was 32 sq.in. ... It was adapted for fitting on the end of the arm in both directions, . . . It was also contrived to incline the surface in any degree to the direction of motion, to try the resistance at all angles of inclination. When fitted on with its length in the direction of its arm, the distance of its center from the axis of mo- tion was 53% in.; and the same distance also when fitted on the other way. Experiments were carried on at different inclinations of plate with a velocity of 12 ft. per sec. or 8.2 miles per [6] hour. When attempting to bring the velocity up to 20 ft. per sec. or 13.6 miles per hour, the thread carrying the weight broke. These experiments are recorded under dates of July 24, 25, 31 and Aug. 11. The results ob- tained were tabulated and the well known formula Pn = P (sitfx) l -**co*x-i was deduced. This is sometimes called Unwin's formula, though for what reason is not clear, as Prof. Unwin simply quotes Prof. Hutton's formula approvingly. The Duchemin formula P p 2 sin A 1 + sin* A for inclined surfaces may be said to represent the best knowledge on the subject and is considered the most re- liable formula in use. The pressures obtained are greater than those from the Hutton formula. Col. Duchemin, a French army officer, made his investigations in 1829 and the results were published in 1842 (Bixby).* Consider- able weight has been attached to the work of Col. Duche- min. Weisbach quotes it, as well as most writers since his time. The Duchemin formula was verified by S. P. Langley in 1888. He had erected at the Allegheny (Penn.) Observatory a whirling-table consisting of two symmetrical wooden arms, each 30 ft. long, revolving in a plane 8 ft. above the ground. The motion thus ob- tained was nearly rectilinear, quite in contrast with that from Button's machine of less than 5-ft. radius. He also used velocities up to 100 ft. per sec., or nearly 70 miles per hour. He writes: At the inception of the experiments with this apparatus it was recognized that the Newtonian law, which made the pressure on an inclined surface proportional to the square of the sine of the angle, was widely erroneous. Occasional experiments have been made since the time of Newton to ascertain the ratio of the pressure upon a plane inclined at various angles to that upon a normal plane, but the published *The writer, while obtaining his information first hand from the sources quoted, acknowledges an obligation to a valuable report: Appendix C of the Report of Sept. 29, 1894, of the Special Army Engineer Board as to the Maximum Span Practicable for Suspension Bridges. By W. H. Bixby, Captain (now General) of Engineers, U. S. A. It is really a treatise on wind pressure in engineering construction. It is said only 500 copies were issued. This valuable paper may be found reprinted entire in "Engineering News," Mar. 14, 1895. experiments exhibit extremely wide discordance, and a series of experiments upon this problem seemed therefore, to be necessary before taking up some newer lines of inquiry. It is remarkable that Langley obtained results varying less than 3% from those derived from the Duchemin for- mula. Regarding this he writes : Only since making these experiments my attention has been called to a close agreement of my curve with the formula of Duchemin, whose valuable memoir published by the French War Department, "Memorial de 1'Artillerie" No. V, I regret not knowing earlier. Attention is called to the monographs by Langley, Experiments in Aerodynamics and The Internal Worlc of the Wind, being Numbers 801 and 884 of the "Smith- sonian Contributions to Knowledge." WIND PEESSUKE ON NONPLANAR SURFACES When the wind blows on nonplanar surfaces the pres- sure on the projected area depends upon the form of the surface. This is important in the case of the cylinder (standpipes, chimneys and similar objects). Rankine states in his Applied Mechanics, "The total pressure of the wind against the side of a cylinder is about one-half of the total pressure against a diametral plane of that cylinder." A theoretical value of two-thirds is found in some treatises, but in engineering practice one-half is generally used. Goodman in his Mechanics Applied to Engineering, London, 1904, gives the following ratios of pressure: Plat plate 1.0 Sphere 0.36 to 0.41 Elongated projectile 0.5 Cylinder 0.54 to 0.57 Wedge (base to wind) 0.8 to 0.97 Wedge (edge to wind) 0.6 to 0.7 Vertex angle 90 Cone (base to wind) 0.95 Cone (apex to wind) Vertex angle 90 0.69 to 0.72 Vertex angle 60 0.54 Lattice girders about 0.8 WIND PRESSURE ON PARALLEL PLATES The pressures upon parallel plates or bars with an open space between them are important in application to plate- girder bridges, the trusses in a truss bridge, or parallel bars in the same truss when one bar is behind another. [8] The Committee of the National Physical Laboratory, England, having decided that one of the first researches to be undertaken in the Engineering Laboratory should be the investigation of the distribution and intensity of the pressure of wind on structures, an elaborate series of experiments was conducted by Thomas Edward Stanton and the results embodied in two papers contributed by him to the Institution of Civil Engineers: "On the Ke- sistance of Plane Surfaces in a Uniform Current of Air" and "Experiments on Wind Pressure." For circular plates 2 in. in diameter at 1% diameters apart, he found the value of the total pressure was less than 75% of the resistance on a single plate; at 2.15 diameters apart the total pressure was equal to that on a single plate; while at a distance of 5 diameters apart the total pressure was 1.78 times that on a single plate. Stanton's first experi- ments were criticized because they were conducted with such small models. For his second series he built a tower and used larger surfaces, but found little to change his previous conclusions. Baker's experiments at the Forth Bridge led him to the conclusion that in no case was the area affected by the wind in any girder which had two or more surfaces ex- posed more than 1.8 times the area of the surface directly fronting the wind. The Board of Trade regulations under which the Forth Bridge was built required that a wind pressure of 56 Ib. per sq.ft. should be used in cal- culations, and this twice over the area of the girder sur- face exposed.* MEASURING WIND PRESSUBE AND VELOCITY It has been assumed by experimenters that the pressure of the wind on a given shape with a certain velocity is the same as that of the shape moving through the air with an equal velocity. This seems to follow from Newton's Corollary V to his Laws of Motion, "The motions of bod- ies included in a given space are the same among them- selves, whether that space is at rest or moves uniformly forward in a right line without any circular motion." *Engineers regard the requirement of 56 Ib. as needless and excessive. [ 9 ] Perhaps the only dissonant voice is that of T. Claxton Fidler, who in his Bridge Construction writes: "But it has not yet been ascertained that the pressure of the wind is the same thing as the resistance offered by the air to a moving body." The pressure of the wind has been measured direct and independently of the velocity. The methods of doing this are so limited in their application that the pressure is almost universally determined in terms of the velocity. Hence, the prime importance of measuring the velocity of the wind correctly. Attempts to do this have been made by all manner of means for the past two centuries. The science of Anemometry has a literature of its own. The velocities obtained by all methods are more or less in error some of them very much so. At present the Kobinson Cup Anemometer or some modification of it is used pretty generally throughout the meteorological world for measuring wind velocities. In the Transactions of the Royal Irish Academy, Vol. XXII, part III (1852), is a paper: "Description of an Improved Anemometer for Registering the Direction of the Wind, and the Space Which it Traverses in Given In- tervals of Time. By the Rev. Tfhomas] R[odney] Rob- inson, D.D., Member of the Royal Irish Academy, and of other Scientific Societies. Read June 10, 1850." Dr. Robinson, who was connected with the observatory at Armagh, Ireland, writes : After some preliminary experiments I constructed in 1843 the essential parts of the machine, a description of which I now submit to the Academy, and I added in subsequent years such improvements as were indicated by experience. It was complete in 1846, when I described it to the British Association at Southampton. He found "from sixteen experiments made in four days with winds from a moderate breeze to a hard gale, -4.011 or, in round numbers, the action on the concave is four times that on the convex." From this he found the theoretic value m of the ratio of the velocity of the wind to that of the cup center to be m = 3.00. Dr. Robinson concluded that no matter what the size of the cups or the [10] lengths of the arms, "the centers of the hemisphere move with one-third of the wind's velocity, except so far as they are retarded by friction." This has been disproved. As a necessary result, many published velocities are in error. The U. S. Weather Bureau prescribes that each pat- tern of anemometer should have its particular law of ro- tation determined by special experiment. Its stand- ard instruments in use throughout the United States have hemispherical cups 4 in. in diameter on arms 6.72 in. long from the axis to the center of the cups. To the ob- served velocity the correction Log. V = 0.509 + 0.912 Log. v is applied in which V is the actual velocity of the wind and v is the linear velocity of the cup centers, both expressed in miles per hour. EFFECT OF VABIATIONS WITHIN THE WIND Measurements of either wind velocity or wind pressure are complicated enormously by the variations in the wind. This is illustrated by two observed facts, both of which are vitally important to the structural engineer : 1. Wind pressures are less per unit of area for large surfaces than for small ones. On the Forth Bridge two pressure boards were set up, one 20 ft. long by 15 ft. high, and 8 ft. from it a circular plate of 1% sq.ft. area. The maximum pressure registered on the small plate dur- ing the years 1884 to 1890 was 41 Ib. per sq.ft. The large board showed at the same time a pressure of 27 Ib. per sq.ft. The readings for the large board never exceeded 80% of those recorded for the small plate at the same time, and generally were 50 to 70%. A technical journal of the time hastily drew the inference from these experi- ments that pressure per square foot varies inversely as area, the velocity remaining the same another illus- tration of generalizing from insufficient data ! 2. Wind velocity increases with the distance from the ground. Thomas Stephenson from his experiments writes the equation or [11] A limiting unit of height must be established for this equation to be of any use. An anemometer placed at the top of the Eiffel Tower, an elevation of 994 ft., and another in the meteorological office at an elevation of 69 ft., showed for light winds velocities nearly four times as great at the top of the tower as at the office. For higher winds the velocities came nearer together. CONCLUSION Cavallo, previously quoted, wrote, "a great many more experiments must be instituted by scientific persons be- fore the subject can be sufficiently elucidated." More than a hundred years after Cavallo's writing, the U. S. Weather Bureau in its monograph on Anemometry, after giving values for pressures and velocities with all the refinements at its command, says : Great dependence cannot be placed in these values for indicated velocities beyond 50 or 60 miles per hour, as thus far direct experiments have not been made at the higher velocities, though it is probable the corrected values are throughout much more accurate than values computed from older formulas and uncorrected wind velocities. Structures have long been designed with satisfactory results to withstand wind pressure. The bracing at times may have been excessive, but in the absence of better knowledge on the subject, engineers cannot radically de- part from present practice. II Wind Stresses in Steel Mill- Buildings SYNOPSIS Discusses the distribution of wind pressure on a sloping roof, referring to the experi- ments of Irminger, Kernot, Stanton, Smith and others. Analyses of stresses in Fink roof trusses show that a uniform vertical excess load is suffi- cient to take care of wind stresses if rigid mem- bers are used. In kneebraced mill-building bents, wind corrections are necessary. Suction effects are to be neglected except as regards anchorage. Recommends wind pressures and unit stresses, and discusses special bracing. In designing ordinary mill-buildings it is common practice either (1) to neglect the wind stresses or (2) to calculate them in accordance with some textbook method and then tone down the results. In doing the latter, the general practice of designing buildings is followed, in conformity to which structures have been built that have rendered excellent service for many years. To bridge the gap between theory and practice, recourse is being had by some to what might be called a new school, which has advanced new methods and new experimental results. In the present article this school will be briefly reviewed, its conclusions negatived, and textbook assumptions made to agree as near as possible with actual conditions the object being to present a safe, sane, workable method of determining and making provision for the wind stresses in steel mill-buildings. AMOUNT AND DISTRIBUTION OF WIND STRESSES A recent writer 1 of the new school states the case thus : In a high wind the maximum pressure against the roof is at the windward eaves. The pressure decreases upward on the windward slope, and is zero, it is claimed, at a point ^'Insurance Engineering," August, 1912. [ 13 ] three-fourths the distance to the ridge. Beyond the zero point, up to the ridge and down the leeward slope, the pres- sure is negative. The wind deflected upward by the wind- ward surface of the roof rarefies the air over the leeward surface, which allows the air inside the building to exert an upward pressure in excess of the downward pressure on the roof. In other words, there is direct or inward pressure on the windward slope of the roof, center of pressure below middle of slope, and at ridge and on all of leeward slope, there is outward pressure or suction. SUCTION ON EOOF In 1894, J. 0. V. Irminger, manager of the Copen- hagen Gas Works, made a number of experiments on wind pressure, the description and results of which he em- bodied in a paper 2 to which reference is often made. A rectangular opening about 6%xll in. was made in a chimney 5 ft. in diameter and 100 ft. high. Into this opening was inserted a conduit 4%x9 in., polished on the inside to reduce friction. Currents of air were made to strike plates and models placed in this conduit and the resultant pressure registered. A model of a pitched roof with 45 slopes showed a normal uplift on the leeward side due to suction three times as great as the normal pressure on the windward side. The conclusion drawn was "if the author's experiments on models represent the facts with regard to buildings, the methods with which roof principals are commonly calculated for wind-pres- sure need revision." An enthusiastic admirer of Irminger writes, 3 "It will be due to him that we surely in the future shall save tons of material in our roofs." In 1891-94, Prof. W. C. Kernot, of the University of Melbourne, made the experiments connected with his name. 4 By means of a gas engine and propeller, he dis- charged a jet of air 12 in. by 10 in., placing into this jet the plates and models he wished to test. He concluded that the usual method of calculating wind stresses in roofs applied only to roofs supported by columns under which the air could blow freely. With roofs of a low 2 "Engineering News," Feb. 14, 1895; "Engineering," Dec. 7, 1895; Proc. Inst. Civ. Engrs., Vol. CXVIII, p. 468. Theodore Nielsen, "Engineering," Oct. 9, 1903. *"Engineering Record," Feb. 10, 1894; Proc. Inst. Civ. Engrs., Vol. CLXXI, p. 218; Australian Association for the Advancement of Science, Vol. V (1893), p. 573, Vol. VI (1895), p. 741. [14] pitch resting on walls having parapets, he found a tend- ency to an uplift. In 1893 and later, T. E. Stanton, of the National Phys- ical Laboratory, England, made the experiments which have become widely known from the papers he contrib- uted to the Institution of Civil Engineers. 5 From ob- servations on models of roofs the sides of which were 3 in. by 1 in. and sloped at 30, 45 and 60, placed in a current of air having velocities of 10.0, 13.6 and 16.8 miles per hour, he writes, "The experiments appear to indicate beyond question the importance of a consider- ation of a negative pressure on the leeward side of roofs/' From later experiments on pressure boards 5x5 ft. to 10x10 ft., he found the coefficients of wind pressure to be as follows : STANTON'S COEFFICIENTS k IN FORMULA Pn = kV 2 (a) Roof mounted on columns through which air can pass 60 45 30 Windward side +0.0034 +0.0028 +0.0015 Leeward side negligible (b) Roofs of buildings in which the pressure on the interior may be affected by the wind. 60 45 30 Windward side +0.0034 +0.0028 +0.0015 Leeward side 0.0032 0.0022 This coefficient gives the normal pressure on roof sur- face in Ib. per sq.ft., if V is the wind velocity in miles per hour, the wind blowing horizontal. Prof. Albert Smith in a paper read before the West- ern Society of Engineers, November, 1910, entitled > bgoocxo - ++++ * + bo" 5 ." 5 ." 5 .-! QO sTTTT * g ,.,00000 ^ oo "7777 * 00 7! TT7 d 3 ^ SB * C 6 ? -J s * r 1 T "! T "! m*"^^ r-OOOOQ 2 OrHiHtH ^r^iHiH S 1-1 ^ . 1 7 T 7 E 3 ^ 34.2 456 342 (5.1) (3.0) (0.9) 1 < s 45 O 60.0. ^50 (5.1) (3.0) (0.9) ' *^ *o VJ 4 3 Id 53 744 55.6 (5.1) (3.0) (0.9) ) W) } >- *" llt.O 74.0 fff.O 3V \FLOOK . (4.5) 130. (3.0) 120.0 q vo (,.5) O 180.0 ' A 1 (6.0) (4.0) (2.0) 1 I 5 I O 1 <-"^-> <.... A eV -> <-/^"> /V ty FLOOR . & c METHOO H FIG. 7. RECTANGULAR BUILDING-FRAME: DIRECT AND BENDING STRESSES CALCULATED BY APPROXIMATE METHOD II 120.0 = Bending moment of 120,000 ft.-lb. (4.0) = Direct stress of 4000 Ib. Taking any aisle we find the direct stress in the fifth- X 42' story columns to be \ + (^,X 30\ pf9 X 6) 16 . 10,^50 The direct stresses coming upon any interior column [68] from the adjacent aisles are equal in amount but op- posite in direction. Hence their algebraic sum is zero i i B C METHOD H FIG. 8. COLUMN-SHEARS AND GIRDER MOMENTS AT SIXTH FLOOR, CALCULATED BY METHOD II and only the outside columns have direct stresses. This may be found directly for any story, say the sixth, (4000 X 30) + (6000 X 18) + (6000 X 6) divided by 48 = 5500 Considering in detail, as in Method I, the sixth floor, we have in Fig. 8 the direct stresses and shears in the columns. The shear in each girder is 10,250 - - 5500 = 4750. The equations for bending moments in the girders can be written as follows : M, = [(4000 X6)X (5500X6) M 3 = [(4000 X6) +(5500 X6) M 3 = [2(4000 X6) +(5500 X6) M 4 = [2(4000X6) +(5500X6) M 5 = [3(4000 X6) +(5500 X6) M 6 = [3(4000 X6) +(5500 X6) [(10,2505500) X16 [(10,2505500) X16 [(10,2505500) X32 [(10,2505500) X32 [(10,2505500) X48 = +57,000 ft.-lb. = 19,000 ft.-lb. = +38,000 ft.-lb. 38,000 ft.-lb. = +19,000 ft.-lb. = 57,000 ft.-lb. The bending moment at the sixth-floor girder of each sixth-story column is 4000 X 6 = 24,000 ft.-lb., and of each fifth-story column is 5500 X 6 = 33,000 ft.-lb. The compression in the floor girders is 6000 1500 = 4500 between Cols. A and 5, 4500 1500 = 3000 be- tween B and C, and 3000 1500 = 1500 between C and D. General equations can easily be deduced which will simplify the calculation of stresses and moments for other floors. If the spaces between columns are unequal, the direct stresses from adjacent aisles will be unequal. This difference is a direct stress in the column between the two aisles considered. If the columns have differ- [69] ent sectional areas, the horizontal shear taken by each column will be in proportion to its moment of inertia. METHOD II-A This is a special case of Method II and may be called 4.0 ROOF 6.0 6.0 6.0 6.0 6.0 6.0 (333; .0$ (0.67) > 14.0 /4.tf 140 (5.0) (3.^ (1.0) 1 fc 1 ^ > ^ 26.0 26.0 26.0 (5.0) 58.0 (2.0) 58.0 (1.0) 58.0 (5.0) p.o) d.o) I 1 S >- 50.0 500 50.0 (5.0) (5.0) d.o) s * 1 1 > 62.0 6^ 6^.^7 (5.0) '^ Q.o) >- 74.0 74.0 74.0 (5.0) (3-0) d.o) 1 a 1 *3 /^. < /6' > 8 T -"FLOOR ^ ^ FLOOR y __. y ^ FLOOR 7 -* FLOOR v 4^ FLOOR A~~ Y 3^ FLOOR v ^ FLOOR ^ ^ t . is FLOOR METHOD Z-A FIG. 9. EECTANGULAK BUILDING-FEAME : DIRECT AND BENDING STRESSES CALCULATED BY APPROXI- MATE METHOD II A 120.0 = Bending moment of 120,000 ft.-lb. (4.0) = Direct stress of 4000 Ib. [70] the Portal Method. The structure is regarded as equiva- lent to a series of independent portals. The total hori- zontal shear on any plane is divided by the number of aisles instead of by the number of columns as in II. An outer column thus takes but one-half the shear of an in- terior column. The stresses and maximum bending mo- ments for a cross-section of the building are as given in Fig. 9. For equal spacing the direct or vertical axial stress due to the overturning moment of the wind is all taken by the outside columns and is the same in amount as in Method II. Considering in detail the sixth floor, we have in Fig. 10 the direct stresses and shears in the columns. 1^ FLOOR 16000^ 6000^ 7,333 5333 333 667 6 r *FLOOR $,667 r SV FLOOR A B <_ METHOD 3-A FIG. 10. COLUMN-SHEARS AND GIRDER MOMENTS AT SIXTH FLOOR, CALCULATED BY METHOD II-A The shear in each girder is 10,250 -- 5500 = 4750. The equations for bending moments in the girders are as follows : M t = [(2,667 X 6) 4- (3,667 X 6)] = 438,000 M, = [(2,667 X 6) 4 (3,667 X 6) (10,250 5,500) X 16] = 38,000 M, = [(2,667 X 6) 4 (3,667 X 6) 4 ( 5,333 X 6) + (7,333 X 6) (10,250 5,500) x 16] = 4 38,000 M 4 = [(2,667 X 6) + (3,667 X 6) + ( 5,333 X 6) 4 (7,333 X 6) (10,250 5,500) X 32] = 38,000 M, = [(2,667 X 6) 4 (3,667 X 6) 4 2( 5,333 X 6) 4- 2(7,333 X 6) (10,250 5,500) X 321 = 4 38,000 M 6 = 1(2,667 X 6) 4 (3,667 X 6) + 2( 5,333 X 6) 4 2(7,333 X 6) (10,250 5,500) X 481 = 38.COO The bending moment at the sixth-floor girder of each outer sixth-story column is 2667 X 6 = 16,000 ft.-lb., and of each inner sixth-story column is 5333 X 6 = 32,000 ft.-lb. At the fifth-floor girder the bending mo- ment of each fifth-story outer column is 3667 X 6 = 22,000 ft.-lb. and of each fifth-story inner column is 7333 X 6 = 44,000 ft.-lb. [71] The compression in the floor girders is 6000 1000 = 5000 between Cols. A and B, 5000 2000 = 3000 be- tween B and C, and 3000 2000 = 1000 between C and D. H H FIG. 11. CROSS-SECTION OF COLUMNS IN TRANSVERSE BENT It is noted from the above that the bending moment in an outer column is one-half that in an interior column; that the point of contraflexure of each girder is at its center; and the bending moments due to wind for all girders of any transverse bent on the same floor are alike. This is an ideal condition for the detailer and the shop. The designer finds this method very simple and his work easily checked. The bending moment in a girder is the mean between the bending moments in the interior col- umn above and below the girder. The width of the aisle does not affect the value of the bending moment.* Methods I and II-A are specially adapted to transverse bents when the columns are turned as in Fig. 11; also when the outer columns carry floor loads only and the stresses are but one-half those of the inner columns. METHOD III This may be called the Continuous Portal Method. The direct stresses in the columns are assumed to vary as their distances from the neutral axis, and the horizontal shear on any plane is equally distributed among the columns cut by that plane. Stresses and maximum bend- ing moments for a cross-section of the building are as given in Fig. 12. The direct stresses in the columns are found the same way and are the same in amount as in Method I. *Burt, "Steel Construction" Section, Wind Bracing. Considering in detail the sixth floor, we have in Fig. 13 the direct stresses and shears in the columns. The shear in the girder A to B and the girder C to D is 9225 4950 = 4275. The shear in the girder B to C is (9225 4950) + (3075 1650) = 5700. 4.0 6.0 6.0' 6.0 6.0 6.0 6.0- 8.0' 6.0 48 6.0 (3.0) (2.0) M 5f ^f\ q o | o ^O 21.0 16.8 zt.o (4.5) (3.0) (1.5) s Q uj 39.0 3I.Z 390 (4.5) (3.0) (l.5) ? 1 s 57.0 45.6 57.O 75.0 (3.0) (1.5) s ^ O K 600 75O (45) (f.5) "^ ^ S 6 V *) ""^T Ci o i i t /44.O I6O.O (4.0) (2.0) o ! <-.-, & '-o'~- s JgV ^ 2.)LJ5WaL. ^ METHOD Ht FIG. 12. EECTANGULAR BUILDING-FEAME : DIEECT AND BENDING STRESSES CALCULATED BY APPROXIMATE METHOD III 144.0 = Bending moment of 144,000 ft.-lb. (4.0) = Direct stress of 4000 Ib. The equations for bending moments in the girders can be written as follows : Mj = [(4000 X6) +(5500 X6) = +57,000 ft.-lb. M, = [(4000X6) +(5500X6)1 [(9225^950) X16] = 11,400 ft.-lb. M, = 2[(4000X6) +(5500X6)] [(9225 4950) X 16] = +45,600 ft.-lb. 2[(4000X6) +(5500X6)] [(9225-^950) X32] [(3075 1650) X16] = 45,600 ft.-lb. 3[(4000X6) +(5500X6)] [(9225 4950) X32] [(3075 1650) X16] = + 11,400 ft.-lb & M 8 B. 3[(4000X6) +(5500X6)] [(9225 4950) X48] [(3075 1650) X32] + [(30751650) X16] = 57,000 ft.-lb. The bending moment at the six-floor girder of each sixth-story column is 4000 X 6 = 24,000 ft.-lb., and of 6000 5500 to 7* FLOOR 6 r - FLOOR A i B 1C METHOD 3H & fvnoo* !D FIG. 13. COLUMN-SHEARS AND GIRDER MOMENTS AT SIXTH FLOOR, CALCULATED BY METHOD III each fifth-story column is 5500 X 6 = 33,000 ft.-lb. The compression in the floor girders is 6000 1500 = 4500 Ib. between Cols. A. and B, 4500 1500 = 3000 between B and C, and 3000 1500 = 1500 between C and D. If the columns are unequally spaced or their sectional LOAD JUV&DZAD) 6VFLOOR FIG. 14. GRAPHICAL COMBINATION OF MOMENTS FROM VERTICAL LOADS AND WIND LOADS IN FLOOR GIRDER areas are different, the location of the neutral axis must first be found. The direct stresses in the columns will vary both as their distances from the neutral axis and [ M] their sectional areas. The horizontal shears taken by the columns will vary as their moments of inertia. CONCLUSION It can be said of each of the above methods of calculat- ing wind stresses that it is easily workable; and to quote Prof. W. H. Burr : "So long as the stresses found by one legitimate method of analysis are provided for, the sta- bility of the structure is assured." At the present time Method I is probably more used than any of the others, though Methods II and II-A have been used quite exten- sively. In the 36-story Equitable Building of New York City, the largest office building in the world, Method I was followed. In its near neighbor, the 32-story Adams Express Building, Method II-A was used. Method III is found in some text-books; it has been used but little about New York, and only to a limited extent elsewhere. The writer personally prefers Method I, though during the past ten years he has used I, II, and II-A. In a 20- story building in Philadelphia built in 1914-1915 he used I. In an 18-story building in Atlanta, designed in 1912, he used II-A. To Method III he objects not only because of its practical limitations but because in theory it seems farther from the truth than any of the others especially when it comes to distributing the shear for bents in build- ings more than four aisles wide. The practice of the writer in calculating wind stresses, using Methods I or II-A (preferably I), is first to find the distance of each column from the neutral axis of the transverse bent to which it belongs, and then to assume the moments of inertia of the inner columns in that bent to be the same and of the outer columns to be one-half that of the inner. The columns are proportioned for all stresses coming upon them, including both direct and cross-bending due to wind. It is seldom that corrections are made for moments of inertia that differ from the as- sumptions. It is often convenient to assume the wind loads on the basis of using the same unit-stresses as for live- and dead- loads. A number of building codes call for a horizontal wind pressure of 30 Ib. per sq.ft. and allow unit-stresses [75 ] to be increased 50% for wind-bracing. A wind load of 30 Ib. per sq.ft. with unit-stress of 24,000 Ib. per sq.in. is equivalent to a load of 20 Ib. per sq.ft. with a unit-stress of 16,000 Ib. per sq.in. the working stress generally used for live- and dead-loads. The diagrams of moments for any floor girder can easily be combined in one figure (see Fig. 14), and the total moment at any point read by scal- ing. Fig. 14 is drawn for beam with ends supported. If the ends were considered fixed the beam would be re- strained and the diagram for both wind and floor loads would show smaller bending moments. Any saving thus made is doubtful economy as in actual practice it is un- certain to what extent the beams are fixed (under vertical load). The building should be examined for wind in a longi- tudinal direction as well as transversely and calculations made if necessary. This is a simple thing to do but in some marked instances it has been neglected. Special attention should be given the column splices, and the connection of floor girders to columns. It is folly to add material to columns or floor girders to meet stresses and moments due to wind, and then neglect their connec- tions. Care should be taken that in all cases the connec- tions are made strong enough for the bending moments coming upon them. Many buildings have main members sufficient to meet wind stresses without efficient connec- tions. 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