THE MECHANICAL PROPERTIES OF WOOD INCLUDING A DISCUSSION OF THE FACTORS AFFECTING THE MECHANICAL PROPERTIES, AND METHODS OF TIMBER TESTING
TEXT
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| SPEED-STRENGTH MODULI AND RELATIVE INCREASE IN STRENGTH AT RATES OF FIBRE STRAIN INCREASING IN GEOMETRICAL RATIO. (Tiemann, _loc. cit._) |
| (Values in parentheses are approximate) |
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| Rate of fibre strain. | | | | | | | |
| Ten-thousandths inch | 2/3 | 2 | 6 | 18 | 54 | 162 | 486 |
| per minute per inch | | | | | | | |
|-------------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------|
| C | Speed of crosshead. | | | | | | | |
| O | Inches per minute | 0.000383 | 0.00115 | 0.00345 | 0.0103 | 0.0310 | 0.0931 | .279 |
| M | | | | | | | | |
| P |---------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------|
| R | Specimens | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All |
| E |---------------------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------|
| S | Relative | | | | | | | | | | | | | | | | | | | |
| S | crushing | | 100.0 | 100.0 | 100.0 | 103.4 | 100.8 | 101.5 | 107.5 | 102.7 | 103.8 | 113.9 | 105.5 | 107.9 | 121.3 | 108.3 | 116.4 | 128.8 | 110.0 |118.9 |
| I | strength | | | | | | | | | | | | | | | | | | | |
| O | | | | | | | | | | | | | | | | | | | | |
| N | Speed-strength | | 0.017 |(0.006)|(0.009)| 0.033 | 0.012 | 0.016 | 0.047 | 0.021 | 0.029 | 0.053 | 0.027 | 0.039 | 0.060 | 0.023 | 0.049 |(0.052)|(0.015)|(0.040)|
| | modulus, _T_ | | | | | | | | | | | | | | | | | | | |
|---+---------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------|
| | Speed of crosshead. | | | | | | | |
| | Inches per minute | 0.0072 | 0.0216 | 0.0648 | 0.194 | 0.583 | 1.75 | 5.25 |
| B | | | | | | | | |
| E |---------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------+-----------------------|
| N | Specimens | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All | Wet | Dry | All |
| D |---------------------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------+-------|
| I | Relative | | | | | | | | | | | | | | | | | | | | | |
| N | crushing | 97.4 | 99.0 | 98.2 | 100.0 | 100.0 | 100.0 | 105.1 | 102.1 | 103.7 | 111.3 | 105.8 | 108.1 | 117.9 | 108.6 | 112.7 | 123.7 | 109.6 | 116.3 | 126.3 | 110.3 | 118.9 |
| G | strength | | | | | | | | | | | | | | | | | | | | | |
| | | | | | | | | | | | | | | | | | | | | | | |
| | Speed-strength |(0.014)|(0.005)| 0.012 | 0.033 | 0.014 | 0.026 | 0.049 | 0.026 | 0.037 | 0.053 | 0.033 | 0.038 | 0.049 | 0.014 | 0.035 | 0.038 | 0.006 | 0.025 |(0.023)|(0.004)|(0.014)|
| | modulus, _T_ | | | | | | | | | | | | | | | | | | | | | |
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| NOTE.--The usual speeds of testing at the U.S. Forest Service laboratory are at rates of fibre strain |
| of 15 and 10 ten-thousandths in. per min. per in. for compression and bending respectively. |
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BENDING LARGE BEAMS
_Apparatus_: A static bending machine (described above), with a
special crosshead for third-point loading and a long platform
bearing knife-edge supports, is required. (See Fig. 29.)
[Illustration: FIG. 29.--Static bending test on large beam. Note
arrangement of wire and scale for measuring deflection; also
method of applying load at "third-points."]
_Preparing the material_: Standard sizes and grades of beams and
timbers in common use are employed. The ends are roughly squared
and the specimen weighed and measured, taking the
cross-sectional dimensions midway of the length. Weights should
be to the nearest pound, lengths to the nearest 0.1 inch, and
cross-sectional dimensions to the nearest 0.01 inch.
_Marking and sketching_: The butt end of the beam is marked _A_
and the top end _B_. While facing _A_, the top side is marked
_a_, the right hand _b_, the bottom _c_, the left hand _d_.
Sketches are made of each side and end, showing (1) size,
location, and condition of knots, checks, splits, and other
defects; (2) irregularities of grain; (3) distribution of
heartwood and sapwood; and on the ends: (4) the location of the
pith and the arrangement of the growth rings, (5) number of
rings per inch, and (6) the proportion of late wood.
The number of rings per inch and the proportion of late wood
should always be determined along a radius or a line normal to
the rings. The average number of rings per inch is the total
number of rings divided by the length of the line crossing them.
The proportion of late wood is equal to the sum of the widths of
the late wood crossed by the line, divided by the length of the
line. Rings per inch should be to the nearest 0.1; late wood to
the nearest 0.1 per cent.
Since in large beams a great variation in rate of growth and
relative amount of late wood is likely in different parts of the
section, it is advisable to consider the cross section in three
volumes, namely, the upper and lower quarters and the middle
half. The determination should be made upon each volume
separately, and the average for the entire cross section
obtained from these results.
At the conclusion of the test the failure, as it appears on each
surface, is traced on the sketches, with the failures numbered
in the order of their occurrence. If the beam is subsequently
cut up and used for other tests an additional sketch may be
desirable to show the location of each piece.
_Adjusting specimen in machine_: The beam is placed in the
machine with the side marked _a_ on top, and with the ends
projecting equally beyond the supports. In order to prevent
crushing of the fibre at the points where the stress is applied
it is necessary to use bearing blocks of maple or other hard
wood with a convex surface in contact with the beam. Roller
bearings should be placed between the bearing blocks and the
knife edges of the crosshead to allow for the shortening due to
flexure. (See Fig. 29.) Third-point loading is used, that is,
the load is applied at two points one-third the span of the beam
apart. (See Fig. 30.) This affords a uniform bending moment
throughout the central third of the beam.
[Illustration: FIG. 30.--Two methods of loading a beam, namely,
third-point loading (upper), and centre loading (lower).]
_Measuring the deflection_: The method of measuring the
deflection should be such that any compression at the points of
support or at the application of the load will not affect the
reading. This may be accomplished by driving a small nail near
each end of the beam, the exact location being on the neutral
plane and vertically above each knife-edge support. Between
these nails a fine wire is stretched free of the beam and kept
taut by means of a rubber band or coiled spring on one end.
Behind the wire at a point on the beam midway between the
supports a steel scale graduated to hundredths of an inch is
fastened vertically by means of thumb-tacks or small screws
passing through holes in it. Attachment should be made on the
neutral plane.
The first reading is made when the scale beam is balanced at
zero load, and afterward at regular increments of the load which
is applied continuously and at a uniform speed. (See SPEED OF
TESTING MACHINE, above.) If desired, however, the load may be
read at regular increments of deflection. The deflection
readings should be to the nearest 0.01 inch. To avoid error due
to parallax, the readings may be taken by means of a reading
telescope about ten feet distant and approximately on a level
with the wire. A mirror fastened to the scale will increase the
accuracy of the readings if the telescope is not used. As in all
tests on timber, the strain must be continuous to rupture, not
intermittent, and readings must be taken "on the fly." The
weighing beam is kept balanced after the yield point is reached
and the maximum load, and at least one point beyond it, noted.
_Log of the test_: The proper log sheet for this test consists
of a piece of cross-section paper with space at the margin for
notes. (See Fig. 32.) The load in some convenient unit (1,000 to
10,000 pounds, depending upon the dimensions of the specimen) is
entered on the ordinates, the deflection in tenths of an inch on
the abscissæ. The increments of load should be chosen so as to
furnish about ten points on the stress-strain diagram below the
elastic limit.
As the readings of the wire on the scale are made they are
entered directly in their proper place on the cross-section
paper. In many cases a test should be continued until complete
failure results. The points where the various failures occur are
indicated on the stress-strain diagram. A brief description of
the failure is made on the margin of the log sheet, and the form
traced on the sketches.
_Disposal of the specimen_: Two one-inch sections are cut from
the region of failure to be used in determining the moisture
content. (See MOISTURE DETERMINATION, above.) A two-inch section
may be cut for subsequent reference and identification, and
possible microscopic study. The remainder of the beam may be cut
into small beams and compression pieces.
_Calculating the results_: The formulæ used in calculating the
results of tests on large rectangular simple beams loaded at
third points of the span are as follows:
0.75 P
(1) J = --------
b h
l (P_{1} + 0.75 W)
(2) r = --------------------
b h^{2}
l (P + 0.75 W)
(3) R = ----------------
b h^{2}
P_{1} l^{3}
(4) E = ---------------
4.7 D b h^{3}
0.87 P_{1} D
(5) S = --------------
2 V
b, h, l = breadth, height, and span of specimen, inches.
D = total deflection at elastic limit, inches.
P = maximum load, pounds.
P_{1} = load at elastic limit, pounds.
E = modulus of elasticity, pounds per square inch.
r = fibre stress at elastic limit, pounds per sq. inch.
R = modulus of rupture, pounds per square inch.
S = elastic resilience or work to elastic limit, inch-pounds
per cu. in.
J = greatest calculated longitudinal shear, pounds per square
inch.
V = volume of beam, cubic inches.
W = weight of the beam.
In large beams the weight should be taken into account in
calculating the fibre stress. In (2) and (3) three-fourths of
the weight of the beam is added to the load for this reason.
BENDING SMALL BEAMS
_Apparatus_: An ordinary static bending machine, a steel I-beam
bearing two adjustable knife-edge supports to rest on the
platform, and a special deflectometer, are required. (See Fig.
31.)
[Illustration: FIG. 31.--Static bending test on small beam. Note
the use of the deflectometer with indicator and dial for
measuring the deflection; also roller bearings between beam and
supports.]
_Preparing the material_: The specimens may be of any convenient
size, though beams 2" X 2" X 30" tested over a 28-inch span, are
considered best. The beams are surfaced on all four sides, care
being taken that they are not damaged by the rollers of the
surfacing machine. Material for these tests is sometimes cut
from large beams after failure. The specimens are carefully
weighed in grams, and all dimensions measured to the nearest
0.01 inch. If to be tested in a green or fresh condition the
specimens should be kept in a damp box or covered with moist
sawdust until needed. No defects should be allowed in these
specimens.
_Marking and sketching_: Sketches are made of each end of the
specimen to show the character of the growth, and after testing,
the manner of failure is shown for all four sides. In obtaining
data regarding the rate of growth and the proportion of late
wood the same procedure is followed as with large beams.
_Adjusting specimen in machine_: The beam should be correctly
centred in the machine and each end should have a plate with
roller bearings between it and the support. Centre loading is
used. Between the movable head of the machine and the specimen
is placed a bearing block of maple or other hard wood, the lower
surface of which is curved in a direction along the beam, the
curvature of which should be slightly less than that of the beam
at rupture, in order to prevent the edges from crushing into the
fibres of the test piece.
_Measuring the deflection_: The method of measuring deflection
of large beams can be used for small sizes, but because of the
shortness of the span and consequent slight deformation in the
latter, it is hardly accurate enough for good work. The special
deflectometer shown in Fig. 31 allows closer reading, as it
magnifies the deflection ten times. It rests on two small nails
driven in the beam on the neutral plane and vertically above the
supports. The fine wire on the wheel at the base of the
indicator is attached to another small nail driven in the beam
on the neutral plane midway between the end nails. All three
nails should be in place before the beam is put into the
machine. The indicator is adjustable by means of a thumb-screw
at the base and is set at zero before the load is applied.
Deflections are read to the nearest 0.001 inch. For rate of
application of load see SPEED OF TESTING MACHINE, above. The
speed should be uniform from start to finish without stopping.
Readings must be made "on the fly."
_Log of the test_: The log sheets used for small beams (see Fig.
32) are the same as for large sizes and the procedure is
practically identical. The stress-strain diagram is continued to
or beyond the maximum load, and in a portion of the tests should
be continued to six-inch deflection or until the specimen fails
to support a load of 200 pounds. Deflection readings for equal
increments of load are taken until well beyond the elastic
limit, after which the scale beam is kept balanced and the load
read for each 0.1 inch deflection. The load and deflection at
first failure, the maximum load, and any points of sudden change
should be shown on the diagram, even though they do not occur at
one of the regular points. A brief description of the failure
and the nature of any defects is entered on the log sheet.
[Illustration: FIG. 32.--Sample log sheet, giving full details
of a transverse bending test on a small pine beam.]
_Calculating the results_: The formulæ used in calculating the
results of tests on small rectangular simple beams are as
follows:
0.75 P
(1) J = --------
b h
1.5 P_{1} l
(2) r = -------------
b h^{2}
1.5 P l
(3) R = ---------
b h^{2}
P_{1} l^{3}
(4) E = -------------
4 D b h^{3}
P_{1} D
(5) S = ---------
2 V
The same legend is used as in BENDING LARGE BEAMS. The weight of
the beam itself is disregarded.
ENDWISE COMPRESSION
_Apparatus_: An ordinary static testing machine and a
compressometer are required. (See Fig. 33.)
[Illustration: FIG. 33.--Endwise compression test, showing
method of measuring the deformation by means of a
compressometer.]
_Preparing the material_: Two classes of specimens are commonly
used, namely, (1) posts 24 inches in length, and (2) small clear
blocks approximately 2" X 2" X 8". The specimens are surfaced on
all four sides and both ends squared smoothly and evenly. They
are carefully weighed, measured, rate of growth and proportion
of late wood determined, as in bending tests. After the test a
moisture section is cut and weighed. Ordinarily these specimens
should be free from defects.
_Sketching_: Sketches are made of each end of the specimens to
show the character of the growth. After testing, the manner of
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The Mechanical Properties of Wood Including a Discussion of the Factors Affecting the Mechanical Properties, and Methods of Timber Testing
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