CIVL 2020 Lab No. 3: Compressive Test of Wood Specimens
CIVL 2020 Lab No. 3: Compressive Test of Wood Specimens
Objectives
Upon successful completion of this lab module, students will be able to:
Set up and perform a laboratory test to determine the mechanical properties of a timber specimen loaded in compression both parallel and perpendicular to the grain.
Record appropriate data from the test and apply safety factors to this data to determine the design compressive stress.
Introduction
When timber is stressed in a manner that causes shortening of the fibers in the direction of the grain, it is identified as:
Compression Parallel to Grain: This occurs when structural studs or posts experience compressive stresses.
Timber exhibits surprising strength in compression parallel to the grain and is efficient as a compression member.
Efficiency Definition: Refers to the strength provided by the member relative to its weight, cost, and ease of installation.
This module focuses on timber subjected to compressive stresses parallel to the grain. Data manipulation allows for the determination of:
Compressive Strength
Modulus of Elasticity
It is essential to recognize that wood is organic and displays variability in its properties compared to concrete and steel.
Wood Structure: Wood resembles a bundle of straws glued together (with lignin) which forms its grain. This structure leads to its classification as an:
Anisotropic Material: This means it behaves differently in different directions.
Example of Anisotropy:
Crushability:
Easier to crush straws when pushed sideways (perpendicular to length).
Harder to crush when pushed along their length (parallel to length).
Compressive Strength Characteristics:
Stronger when loaded parallel to grain compared to perpendicular.
Case Study: A piece of clear Douglas Fir, dimensions 150mm x 38mm x 38mm (6" x 1½" x 1½") tested under:
Force of 112 kN (25,200 lbs) required to crush it when loaded parallel to grain.
For loads applied perpendicular to grain, failure occurred at approximately 20% of the parallel load.
Modes of Failure During Compressive Testing:
Crushing (a): Resulting in horizontal planes of crushed fibers.
Wedge Splitting (b): Characterized by a Y-shaped failure at the specimen's surface.
Shearing (c): Occurring at an angle more than 45 degrees to the load applied.
Splitting (d): Related to specimens with internal defects.
Combined Crushing and Splitting (e): Typically arises in cross-grained pieces.
Brooming (f): Common with elevated moisture content or improperly cut specimen ends.
Important Note: For characterizing defect-free wood, results from failures in modes (d), (e), and (f) are excluded from final data tabulations.
Review
Recollection from lectures regarding:
Modulus of Elasticity (E): Also known as Young's Modulus.
Definition: A measure of a material's stiffness.
Determined by plotting a stress-strain graph and finding the slope of the elastic portion.
Stress-Strain Curve for Timber: Helps in identifying:
Characteristics of brittle or ductile material.
Proportional limit, yield strength, and ultimate strength.
Refer to the textbook (Goodno, section 1.4) for a refresher on this topic.
The Laboratory Test
Test Setup for Parallel-to-Grain Testing:
Utilize a specimen sized 38 mm x 38 mm x 150 mm (may vary slightly).
Mount Select Structural Douglas Fir in a testing machine for parallel load application.
Compressometer: Dial gauge used to measure shortening of the specimen.
Necessary to record changes in length at predetermined load intervals to equate stress and strain.
During the test, take note of:
Rate of movement of the load pointer compared to the compressometer pointer after the load exceeds 40 kN.
The failure mode displayed by the specimen.
Instructor will guide on the setup and procedures for perpendicular-to-grain testing.
The Results
Understanding test results may be challenging due to the organic and non-homogeneous nature of timber, versus the more predictable properties of homogeneous materials like steel.
Instructions for Analyzing Parallel-to-Grain Results:
Calculate stress corresponding to each load reading using the original cross-sectional area of the specimen.
Calculate strain corresponding to each extensometer reading using the original specimen length.
Plot the entire stress-strain curve by hand (no computer) on graph paper.
Determine the modulus of elasticity, proportional limit, and ultimate stress, labeling each point on the graph.
Develop a sketch and description of the failure mechanism as specified in the introduction.
Design Code Value and Safety Factor Calculation:
An allowable stress value for select Douglas Fir is 11.0 MPa.
Assume failure occurred just beyond the proportional limit of the specimen; calculate the corresponding safety factor against this permissible stress and analyze if it is appropriate, explaining your reasoning.
Connection Detail:
Figure presented shows a typical beam-to-column connection detail.
Assumptions:
Steel saddle remains intact.
Bolts carry no load.
Allowable stresses for compression are:
Parallel to grain: 9.7 MPa
Perpendicular to grain: 3.17 MPa
Calculate the magnitude of the load safely transferable between the beam and the column under these conditions.