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-: THESIS :-
TESTS OF STEEL-CONCRETEHE BEAMS.
BY
~
C. M. BLANCHARD ©n, W. C. ARMSTRONG.
Class '03,
THESIS
TESTS OF STEEL-CONCRETE BEAMS,
The object of this set of tests was to determine how well
the results obtained by means of the theory proposed by W. Kendrick
Hatt, of Purdue University would agree with the results obtained by
tests made on beams which were of varied proportions of matrix and
aggregate and of the reinforcing material and which were also maie
unier varied conditions,
Tne beams used in these tests were made in wooden moulds.
Those marked dry and normal in Table I. being thoroughly tamped,
while those marked very wet were tanped but little. Tne >eans were
oc a uniform size, all being six (6) inches square end of sufficient
length to give a span of sevejzty-two (72) incnes between supports,
except beams 52 and 5b which ned a span of thirty-six (36) inches.
The reinforcing material useli consisted of Be and 14"
round rods of mild steel and were aj] placed 1" from tension face
of beam, two being used in eacn beam,
34084
Two differert brands of cement were used (Atlas and Aetna).
the Atlas being a well known svandard brand, and the Aetna, a local
cement which is made at Fenton, Michigan, Tests of standard bri-
quetvtves were :nade on both cements, the results being shown in
Table IV,
All beems were made indoors and were left there until
taken from moulds, which time varied from one to four days accorlin.:
to tne amount of water used in mixing, after which they were set out
doors until tested. Beams were all of gravel concrete, As sand wes
in excess, the gravel was &11 sifted through a sieve of sixteen
meshes to the square inch, all stones larger tha: 1," inch in
iilaneter being rejected, then the sand passing through the sieve and
the stones cauzht by it were mixed with the cement in the ratios (by
volumes) as gnown in Tahle I,
The beams were tested at azes varying from 7 to 64 days
as shown ix Tale II. All of the beans were broken by meens of the
Tinurs Olsen testing machine in the Meshanical Laboratory, wnich the elastic lirit of the reinforcing metal is reeched, he
calls this point the point of failure, But, as all the beams in
these tests failed by crushins of the concrete instead of by breaking
of the rods, the theory proposed by him would hardly apply at the
point of failure for these beans, Wo curves were plotted for beams
Sa end 56 whicn were of plain concrete without reinforcement es the
totel deflection for either wes less than .Q1 of an inch, and the
only value of the tests of these two is to stow to whet s marked
degree tne flexibility of tne beams is increased py tne addition
of the metal reinforceme:t,
The assumptions uoon which the theory proposed by Mr,
Hatt are based are as follows; 1, The cross sections of the beams
remain plain surfaces; 2. Tue applied forces are serpendicular to
the neutral surface of the beam; 3, The values of the moduli of
elasticity obtained in simple tension and comoression tests will
apply to the material in the beans when under flexion; 4, There is
no slipping vcetween the concrete end the reinforcing metal; 5, There
are 10 initial stresses in the beam due to cortraction of tne concrete
(4)
While settinz, The analysis also sucroses the fracture to be due to
bending and not horizontal shear. If the cross sections are assumed
to remain plain surfaces during flexture the distortion of any fibre
wil? be provortional to its distance from the neutral axis, It
follows that the law of variation of stresses will be represented
hy the stress strain diagram shown on curve sheets. ‘These stress
strain diasrams are assumed to be parabolic arcs, This assumption
has becn justified in the case of compressional stress strain dia-
diagram, by a large number of experinents but does not seem to be
so clearly shown in this case,
The quantities used in the formulas for tneoretical
results were as follows:
it
hx distance from compression face to neutral axis.
hu
il
distance from compression face to the center of gravity
of the reinforcement, }
p <= ratio of area of steel to tnat of cross section of beem,
Es, Ec, Et = moduli of elacity of the steel, concrete in com-
7
>ress3ion and concrete tension, respectively.
Ee
n = Et
. 2S
m © Bt
f = stress in metal reinforcement,
(5)
it
c = comvression stress in outer fibre of concrete,
t = tensional stree in outer fibre of concrete assumed to
be 300#.
Ec and Et are measured at tne stresses c and t. The
values x, u and p are ratios; p and u are at the control of the
designer, while x depends on p, u, n and m3;.n and m are fixed by
the quality of the materisls, and they chan:ze during flexure with
varying values of c, f and t; that is, the modulus of elasticity
of the concrete varies with the stress at which it is measured,
For practical purposes of computation, however, the constant values
of n ard mirsy ve used appropriate to the point A and to tne point
of cracking, The values proposed by Prof, Hatt were N= 2 and
m—12 at point A, and n=12 and m= 90 at point of first crack,
and these values were used in computing the results shown in Table
III. On the assumption of plane cross section during flexure we mey
determine the ratio of f to c and f to t in the following formulas
tnx
Cc =-T—x
r- tm(u— x)
il—x
Next, to locate the neutral axis; ie, to determine the value
(6)
of x, we mey ecuete the forces of tersion amd somoression on the
cross section, asswsins, a3 before, t.int the streas strain diagrams
are arcs of parabolas,
£4 ex—*% t(1 — x)+ pf
into which the values of f and c above may be substituted and,
solving for x, we get
24 x*n="/ (1 — x)*&4 pm(u — x)
and, after solving, this reduces to
x= -(4,5)4 “Yan + 5° m + p [6m(u[n — 1)+ 1))
e(n— 1)
Havin:: obtained x we may compute c and f and finally
obtain tne moment of resistance of the section, Taking moments about
the neutral axis, we have
ee pnx” (n — x)*
w= tfh [a (1 — xF + re pp maa]
These equations are to be applied to compute the load at
point A, At the load corresporndin,s to the crackins of the concrete
in the tension face, these equations should be modified to corres-
pong to tne fact that tne stress strein aiagram for the concrete in
tension is more nearly a rectaigle than ea parabola, The differci:c .,
nowever, vevween iene results at the time of the appearance of the
(7)
crack due to the assumption of a rectansle or a perandola is very
small, With proper values of n and m the equations may be allowed
to sterd. When, however, the creck heving formed itself, extends
throughout the lower region of the cross section the equations
must be modified by the omission of tne effect of tensional forces
due to the resistance of concrete under tension, We then have:
nox = pf or p Su —-x)= Sx?
which serves to locate tire neutral axis,
The loéds combuted by the application of tine forezoing
equations are shown in Table III and are to be compared with those
piven in Table II, which are tne loads carried by the been tested.
From an inspection of Tavle II, it may be seen that both
the point A, and point of first crack varied considerably for tne
different beams, but this would be expected, as the beams were vur-
posely made with as meny varying conditions es possible,
The ratio of the greatest to the least value of A Was
as 3:1, and for the voint of first crack less than 2:1, ana dota
cases the theoretical load was a mean between the two, therefore we
may conclude that with a large fa ctor of safety, such as is
(3)
necessarily used in concrete construction due to the fact that
two pieces of concrete made uuder sinilar conditions, do not show
concordant tests, it would be yractical to use these formulas
with the constants here employed for tne design of concrete steel
beams,
(9)
Kind,
TABLA NO, I.
Condition
A 4a
\When made, , After Test, Wee los,
No,
No.
No,
No.
5e ard 5h
No,
No,
No,
No,
No.
No.
No,
Wo.
No,
No,
No.
1.
10.
ll.
12,
13.
14,
15.
16.
O:3:1 Aetna
" n
" "
3:2:1 Atlas
" n
S3se:l1 Aetna
tt n
3:231 Atlas
" "
4:2:1 "
Sre:l "
" "
Biel "
" n
S:2:1 Aetna
i" "
— + -_ - 2.
Rether dry First cracked on
bottom then crumbl- 250
ed on top.
" " Same as No. 1., Also
slivered along rods, 206
" " Crushed on bottom
crumbled on top, O28
" " Cracked on »otvvon
crumoled on too, 250
" " Cracked clear tnrouzh a - 113
glad not crusa. b- lol
Normal Crecked on bottom
then crusned on top, 204
" Cracked on bottom
vhen crusi:ed on tor, el
Very wet Split alonz rods on
hnoalf of beam,. : 259
" " Split alonz roads on
nealf of beam, 260
" " Cracked on Lotrtom
tien crus‘ied on top. 209
" " Split alon= rods on
helf of beem, LOS
" " Cracked on bottom
tien crus:ed on ton, 2 46
" " Cracked on bottom then
crushed on top anda sli- 267
vered short dis, on side
" " Cracked on bottom cruyvi-
led on top ctnen broke 267
out chunck on bottom
Normal Cracked on vottom crush-
ed on top then cracked 255
diasonelly across beam
" Broke neerly strait 299
across,
(10)
TADLE NO. II.
Point A, Crack, Failure,
Bean Kina. Age in Loed Defl. Load | Defl., Load Defl,
No. Days. oounds! inches vounds'inches pounds incnes
1. 61% 7 1,000 0.12 2,000 0.40 2,100 0.75
2. 61% 64 600 0.05 2,800 0.38 $3,000 0,75
3. «61% 64 600 0.05 2,800 0.38 3,000 0.75
4, .61% 28 1,000 0.08 --~---- ~~-- 2,500 0.82
5a, Plein 28. ----- e--- o---- ---- 1,500 0.0068
5b. " £8 9 =nene ean a---- ames 1,300 0,01
6. ~ 61% 31 1,200 0.04 38,400 0.35 38,600 0.90
7. .61% 31 800 0.03 3,200 0.30 3,600 0.74
8, 1.09% 34 9 a--5- ---- 1,800 0.20 2,000 0.41
9. 61% 34 400 0.02 2,200 0.28 2,100 0.32
10. 1,09% 29 600 0.01 1,800 0.19 2,000 0.27
11, 1.09% 29. 1,000 0.12 1,600 0.22 1,800 0.27
12. 1.09% 29 400 0.04 1,800 0,24 2,000 0.£8
13, 1.09% 29 1,000 0.07 3,000 0.29 3,800 0,45
14, 1.09 29 1,000 0.08 2,800 0.28 3,400 0.48
15. 1.09% 25 1,200 0.08 2,200 0.24 2,800 0.49
16, .61% 25 1,200 0.03 2,000 0.18 3,000 0.38
- Se © eee ee ee OO - -e
*" ba abd Ob 3' between supoorts,
(11)
TARL:: NO. III.
Stress per Concrete in
Rein- Loed at sq. in, steel. Comp. Value of x for
forced Point First Point First Point First Point First
per cent A. Crack.
Moment due to weight of Beam to be deduced from theoretical dead
loads.
TABLE NO. IV.
Tensile Strenzth of Standard Briquettes of Atlas Portland Cement,
Neat, 7 days. el days.
" §24 | 640
" O14 622
" 475 635
504.35 6a50