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BALLISTICS (from the Gr. fMXkee)

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Originally appearing in Volume V03, Page 272 of the 1911 Encyclopedia Britannica.
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BALLISTICS (from the Gr. fMXkee)  , to throw), the See also:science of throwing warlike missiles or projectiles . It is now divided into two parts:—Exterior See also:Ballistics, in which the See also:motion of the projectile is considered after it has received its initial impulse, when the projectile is moving freely under the See also:influence of gravity and the resistance of the See also:air, and it is required to determine the circumstances so as to See also:hit a certain See also:object, with a view to its destruction or perforation; and Interior Ballistics, in which the pressure of the See also:powder-See also:gas is analysed in the See also:bore of the See also:gun, and the investigation is carried out of the requisite See also:charge of powder to secure the initial velocity of the projectile, without straining the gun unduly . The calculation of the stress in the various parts of the gun due to the powder pressure is dealt with in the See also:article See also:ORDNANCE . I . EXTERIOR BALLISTICS . In the See also:ancient theory due to Galileo, the resistance of the air is ignored, and, as shown in the article on See also:MECHANICS (§ 13), the trajectory is now a See also:parabola . But this theory is very far from being of See also:practical value for most purposes of gunnery; so that a first requirement is an accurate experimental knowledge of the resistance of the air to the projectiles employed, at all velocities useful in See also:artillery . The theoretical assumptions of See also:Newton and See also:Euler (hypotheses magis mathematicae quam naturales) of a resistance varying as some See also:simple See also:power of the velocity, for instance, as the square or See also:cube of the velocity (the quadratic or cubic See also:law), See also:lead to results of See also:great See also:analytical complexity, and are useful only for provisional extrapolation at high or See also:low velocity, pending further experiment . The See also:foundation of our knowledge of the resistance of the air, as employed in the construction of ballistic tables, is the See also:series of experiments carried out between 1864 and -188o by the Rev . F . Bashforth, B.D . (See also:Report on the Experiments made with the Bash-forth See also:Chronograph, &c., 1865—187o; Final Report, &c., 1878—1880; The Bashforth Chronograph, See also:Cambridge, 1890) .

According to these experiments, the resistance of the air can be represented by no simple algebraical law over a large range of velocity . Abandoning therefore all a priori theoretical See also:

assumption, Bashforth set to See also:work to measure experimentally the velocity of shot and the resistance of the air by means of equidistant electric screens furnished with See also:vertical threads or See also:wire, and by a chronograph which measured the instants of See also:time at which the screens were cut by a shot flying nearly horizontally . Formulae of the calculus of finite See also:differences enable us from the chronograph records to infer the velocity and retardation of the shot, and thence the resistance of the air . As a first result of experiment it was found that the resistance of similar shot was proportional, at the same velocity, to the See also:surface or See also:cross See also:section, or square of the See also:diameter . The resistance R can thus be divided into two factors, one of which is d2, where d denotes the diameter of the shot in inches, and the other See also:factor is denoted by p, where p is the _resistance in pounds at the same velocity to a similar 1-in. projectile; thus R=d2p, and the value of p, for velocity ranging from 1600 to 2150 ft. per second (f/s) is given in the second See also:column of the See also:extract from the abridged ballistic table below . These values of p refer to a See also:standard See also:density of the air, of 534.22 grains per cubic See also:foot, which is the density of dry air at See also:sea-level in the See also:latitude of See also:Greenwich, at a temperature of 62° F. and a barometric height of 30 in . But in consequence of the humidity of the See also:climate of See also:England it is better to suppose the air to be (on the See also:average) two-thirds saturated with aqueous vapour, and then the standard temperature will be reduced to 6o° F., so as to secure the same standard density; the density of the air being reduced perceptibly by the presence of the aqueous vapour . It is further assumed, as the result of experiment, that the resistance is proportional• to the density of the air; so that if the standard density changes from unity to any other relative density denoted by r, then R=rd2p, and T is called the coefficient of tenuity . The factor r becomes of importance in See also:long range high See also:angle See also:fire, where the shot reaches the higher attenuated strata of the See also:atmosphere; on the other See also:hand, we must take r about 800 in a calculation of See also:shooting under See also:water . The resistance of the air is reduced considerably in See also:modern projectiles by giving them a greater length and a sharper point, and by the omission of projecting studs, a factor K, called the coefficient of shape, being introduced to allow for this See also:change . For a projectile in which the ogival See also:head is struck with a See also:radius of 2 diameters, Bashforth puts K=0•975; on the other hand, for a See also:flat-headed projectile, as required at See also:proof-butts, K=1.8, say 2 on the average . For spherical shot K is not See also:constant, and a See also:separate ballistic table must be constructed; but K may be taken as 1.7 on the average .

Lastly, to allow for the See also:

superior centering of the shot obtainable with the See also:breech-loading See also:system, Bashforth introduces a factor e, called the coefficient of steadiness . This steadiness may vary during the See also:flight of the projectile, as the shot may be unsteady for some distance after leaving the muzzle, afterwards steadying down, like a See also:spinning-See also:top . Again, e may increase as the gun wears out, after firing a number of rounds . See also:Collecting all the coefficients, r, e, a, into one, we put (2) R =nd2p=nd2f(v), where and n is called the coefficient of reduction . By means of a well-chosen value of n, determined by a few experiments, it is possible, pending further experiment, with the most See also:recent See also:design, to utilize Bashforth's experimental results carried out with old-fashioned projectiles fired from muzzle-loading guns . For instance, n=o•8 or even less is considered a See also:good average for the modern See also:rifle See also:bullet . Starting with the experimental values of p, for a standard projectile, fired under standard conditions in air of standard density, we proceed to the construction of the ballistic table . We first determine the time See also:tin seconds required for the velocity of a shot, d inches in diameter and weighing w lb, to fall from any initial velocity V(f/s) to any final velocity v(f/s) . The shot is supposed to move horizontally, and the curving effect of gravity is ignored . If At seconds is the time during which the resistance of the air, R lb, causes the velocity of the shot to fall Av(f/s), so that the velocity drops from v+iAv to v—ZAv in passing through the mean velocity v, then (3) Rot =loss of momentum in second-pounds, w(v -{- z Ov)/g —w(v — a 0v) /g = wLv/g so that with the value of R in (1), (4) At = wAv/nd2pg• We put (5) wind2 = C; and See also:call C the ballistic coefficient (See also:driving power) of the shot, so that (6) At = See also:CAT, where (7) AT = Ov/gp, and AT is the time in seconds for the velocity to drop Lv of the standard shot for which C =1, and for which the ballistic table is calculated . Since p is determined experimentally and tabulated as a See also:function of v, the velocity is taken as the See also:argument of the ballistic table; and taking iv = io, the average value of p in the See also:interval is used to determine AT . Denoting the value of T at any velocity v by T (v), then (8) T(v) =sum of all the preceding values of AT plus an arbitrary constant, expressed by the notation (9) T(v) =E(Av)/gp+ a constant, or fde/gp+ a constant, in which p is supposed known as a function of v .

The constant may be any arbitrary number, as in using the table the difference only is required of two See also:

tabular values for an initial velocity V and final velocity v; and thus (to) T(V)—T(v)=1vOv/gp or fvdv/gp; and for a shot whose ballistic coefficient is C (II) t= CfT(V) —T(v)] . To See also:save the trouble of proportional parts the value of T(v) for unit increment of v is interpolated in a full-length extended ballistic table for T . Next, if the shot advances a distance As ft. in the time At, during which the velocity falls from v-I 44ov to v— yav, we have (12) See also:RAs =loss of kinetic See also:energy in foot-pounds w(v+lAv)2/g—w(v—iAv)2/g=wvav/g, so that (13) As=wvOv/nd2pg=CAS, where (14) AS = vLv/gp = vLT, and AS is the advance in feet of a shot for which C = t, while the velocity falls Av in passing through the average velocity v . Denoting by S(v) the sum of all the values of AS up to any assigned velocity v, (15) S(v)=E(OS)+ a constant, by which S(v) is calculated from AS, and then between two assigned velocities V See also:rand v, vvd (16) S(V) -5(v) = vAT = E gvAv p orJ _', and if s feet is the advance of a shot whose ballistic coefficient is C, ' . (17) s=C[S(V) —S(v)] . In an extended table of S, the value is interpolated for unit increment of velocity . A third table, due to See also:Sir W.D . Niven, F.R.S., called the degree table, determines the change of direction of motion of the shot while the velocity changes from V to v, the shot flying nearly horizontally . To explain the theory of this table, suppose the tangent at the point of the trajectory, where the velocity is v, to make an angle i radians with the See also:horizon . Resolving normally in the trajectory, and supposing the resistance of the air to See also:act tangentially, (18) v(di/dt) =g See also:cos i, where di denotes the infinitesimal decrement of i in the infinitesimal increment of time dt . In a problem of See also:direct fire, where the trajectory is flat enough for cos i to be undistinguishable from unity, See also:equation (16) becomes (19) v(di/dt)=g, or di/di=g/v; so that we can put (20) Di/At = g/v, if v denotes the mean velocity during the small finite interval of time i t, during which the direction of motion of the shot changes through Ai radians . If the inclination or change of inclination in degrees is denoted by S or M, (21) 6/18o=i/ir, so that 180 1805 At M = 4i= 7 v and if 6 and i change to D and I for the standard projectile, 2 AT Av 18og AT (3) AI =g v =vp, AD = v , and (24) I(V)-I(v)=Evvpor 'L 7, d ,D(V)-D(v)=t8o]I(V)-I(v)] .

The differences AD and AI are thus calculated, while the valuesof D(v) and I(v) are obtained by summation with the arithmometer, and entered in their respective columns . For some purposes it is preferable to retain the circular measure, i radians, as being undistinguishable from See also:

sin i and tan a when i is small as in direct fire . The last function A, called the See also:altitude function, will be explained when high angle fire is considered . These functions, T, S, D, 1, A, are shown numerically in the following extract from an abridged ballistic table, in which the velocity is taken as the argument and proceeds by an increment of to fjs; the column for p is the one determined by experiment, and the remaining columns follow by calculation in the manner explained above . The initial values of T, S, D, I, A must be accepted as belonging to the anterior portion of the table . In any region of velocity where it is possible to represent p with sufficient accuracy by an empirical See also:formula composed of a single power of v, say the integration can be effected which replaces the summation in (to), (16), and (24); and from an See also:analysis of the See also:Krupp experiments See also:Colonel Zabudski found the most appropriate See also:index m in a region of velocity as given in the following table, and the corresponding value of gp, denoted by f (v)or v'"/k or its See also:equivalent Cr, where r is the retardation .

End of Article: BALLISTICS (from the Gr. fMXkee)
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