IS 1708 Parts 1-18 (1986) specifies standardized methods for testing small clear specimens of timber to determine their physical and mechanical properties. Covering tests such as specific gravity, static and impact bending strength, compressive and tensile strength parallel and perpendicular to grain, hardness, cleavage strength, nail and screw holding power, brittleness, and torsional strength, this comprehensive standard is essential for engineers, researchers, and quality controllers involved in timber evaluation and wood product development.
Overview
IS 1708 Parts 1-18 (1986) specifies standardized methods for testing small clear specimens of timber to determine their physical and mechanical properties. Covering tests such as specific gravity, static and impact bending strength, compressive and tensile strength parallel and perpendicular to grain, hardness, cleavage strength, nail and screw holding power, brittleness, and torsional strength, this comprehensive standard is essential for engineers, researchers, and quality controllers involved in timber evaluation and wood product development.
Audience
Contents
Structure
IS 1708 Part 1-18: Scope - Key Formulas & Tables Summary
The scope covers determination of mechanical characteristics of timber under static bending and impact tests using specified formulae.
| Characteristic | Unit | Formula | Notes |
|---|---|---|---|
| Fibre stress at limit of proportionality (FS) | kg/cm² | ( FS = \frac{3P a}{b h^2} ) | P = load at LP, a = load-support dist. |
| Equivalent fibre stress at max load (Modulus of Rupture) | kg/cm² | ( M_R = \frac{3P' a}{b h^2} ) | P' = max load |
| Modulus of elasticity (E) | kg/cm² | ( E = \frac{3P a l^2}{4 b h^3 \delta} ) | l = gauge length, δ = deflection at LP |
| Horizontal shear stress at LP (neutral plane) | kg/cm² | At ends: ( \frac{3P}{4 b h} ), Center: 0 | |
| Horizontal shear stress at max load | kg/cm² | At ends: ( \frac{3P'}{4 b h} ), Center: 0 | |
| Work to limit of proportionality (elastic resilience) | kg.cm/cm³ | ( W_k = \frac{P \delta l}{2 b h} ) |
| Characteristic | Unit | Formula |
|---|---|---|
| Maximum height of drop (H) | cm | Measured directly |
| Height of drop at LP (H') | cm | From load-deflection curve |
| Fibre stress at LP (impact) | kg/cm² | ( FS = \frac{3 H' W l}{b h^2 \delta} ) |
| Modulus of elasticity (impact) | kg/cm² | ( E = \frac{H' W l^3}{2 b h^3 \delta^2} ) |
| Work to LP |
IS 1708 Part 1-18: Test Specimen Preparation and Dimensions
| Specimen Size | Cross-Section (cm) | Length (cm) | Failure Area (mm) | Failure Plane |
|---|---|---|---|---|
| Large | 5 × 5 | 20 (6 shear) | 50 × 20 | Radial or Tangential |
| Small | 2 × 2 | 8 (3 shear) | 20 × 10 | Radial or Tangential |
This ensures standardized specimen preparation for consistent shear testing results.
IS 1708 Part 1-18: Test Procedures & Loading Rates
| Test Size/Type | Rate of Movable Head (mm/min) | Notes |
|---|---|---|
| Both sizes | 2.5 | Continuous loading until max load |
| Both sizes | 0.6 | Alternative rate |
| Both sizes | 0.4 | Alternative rate |
flowchart LR
Start[Test Setup] --> LoadApplied[Apply Load]
LoadApplied --> MovableHead[Movable Head moves at constant rate]
MovableHead --> MaxLoadReached{Max Load reached?}
MaxLoadReached -- No --> ContinueLoading[Continue at constant rate]
MaxLoadReached -- Yes --> RecordData[Record Load & Displacement]
RecordData --> End[Test Complete]
This ensures compliance with IS 1708 Part 1-18 for consistent and reliable test results.
IS 1708 Part 1-18: Recording of Data and Calculations
| Characteristic | Unit | Formula |
|---|---|---|
| Fibre stress at limit of proportionality (FS at LP) | kg/cm² | ( \frac{3P l}{2 b h^2} ) |
| Equivalent fibre stress at maximum load (Modulus of Rupture, M of R) | kg/cm² | ( \frac{3P' l}{2 b h^2} ) |
| Modulus of Elasticity (M of E) | kg/cm² | ( \frac{P l^3}{4 b h^3 \Delta} ) |
| Horizontal shear stress at LP (HS at LP) | kg/cm² | ( \frac{3P}{4 b h} ) |
| Horizontal shear stress at maximum load (HS at ML) | kg/cm² | ( \frac{3P'}{4 b h} ) |
| Work to LP (elastic resilience) (Wk to LP) | kg·cm/cm³ | ( \frac{C A}{16 h} ) |
| Work to maximum load (Wk to ML) | kg·cm/cm³ | ( \frac{C A'}{l b h} ) |
| Total work | kg·cm/cm³ | ( \frac{C A''}{l b h} ) |
Specific Gravity Determination (IS 1708 Part 1-18)
Specific Gravity at Test Condition: [ \text{Specific Gravity} = \frac{W_1}{V_1} ]
Adjusted Specific Gravity (considering moisture content): [ \text{Adjusted Specific Gravity} = \frac{W_1}{V_1} \times \frac{100}{100 + m} ]
Oven Dry Specific Gravity: [ \text{Oven Dry Specific Gravity} = \frac{W_o}{V_o} ]
flowchart TD
A[Specimen Preparation] --> B{Specimen Size?}
B -->|Rectangular| C[Use 5x5x15 cm or 2x2x6 cm]
B -->|Irregular| D[Take ~10 cm³ volume specimen]
C & D --> E[Measure Weight (W1) and Volume (V1)]
E --> F[Calculate Specific Gravity = W1/V1]
F --> G{Moisture Content Known?}
G -->|Yes| H[Adjusted Specific Gravity = (W1/V1)*(100/(100+m))]
G -->|No| I[Use Specific Gravity at Test]
H & I --> J{Oven Dry Required?}
J -->|Yes| K[
IS 1708 Part 1-18: Static Bending Strength Tests Summary
| Characteristic | Formula | Units |
|---|---|---|
| Fibre Stress at Limit of Proportionality (FS at LP) | ( \sigma = \frac{3 P l}{2 b h^2} ) | kg/cm² |
| Modulus of Rupture (Equivalent fibre stress at max load) | ( \sigma = \frac{3 P' l}{2 b h^2} ) | kg/cm² |
| Modulus of Elasticity (M of E) | ( E = \frac{P l^3}{4 b h^3 \delta} ) | kg/cm² |
| Horizontal Shear Stress at LP (HS at LP) | ( \tau = \frac{3 P}{4 b h} ) | kg/cm² |
| Horizontal Shear Stress at Max Load (HS at ML) | ( \tau = \frac{3 P'}{4 b h} ) | kg/cm² |
| Work to LP (Elastic Resilience) | ( W_k = \frac{C A}{16 h} ) | kg·cm/cm³ |
| Work to Max Load | ( W_k = \frac{C A' l b h}{1} ) | kg·cm/cm³ |
| Total Work | ( W = \frac{C A'' l b h}{1} ) | kg·cm/cm³ |
Impact Bending Strength Test (IS 1708 Part 1-18)
| Characteristic | Formula | Unit |
|---|---|---|
| Fibre stress at limit of proportionality (FS at LP) | ( \frac{3Pl}{2bh^2} ) | kg/cm² |
| Equivalent fibre stress at max load (Modulus of Rupture, M of R) | ( \frac{3P'l}{2bh^2} ) | kg/cm² |
| Modulus of Elasticity (M of E) | ( \frac{P l^3}{4 b h^3 \delta} ) | kg/cm² |
| Horizontal shear stress at LP (HS at LP) | ( \frac{3P}{4bh} ) | kg/cm² |
| Horizontal shear stress at max load (HS at ML) | ( \frac{3P'}{4bh} ) | kg/cm² |
| Work to LP (Elastic resilience) | ( \frac{CA}{16h} ) | kg·cm/cm³ |
| Work to max load | ( \frac{CA' l b h}{1} ) | kg·cm/cm³ |
| Total work | ( \frac{CA'' l b h}{1} ) | kg·cm/cm³ |
Where:
| Characteristic | Unit | Formula | Description |
|---|---|---|---|
| Compressive stress at limit of proportionality (CS at LP) | kg/cm² | ( CS_{LP} = \frac{P}{A} ) | (P): Load at limit of proportionality (kg), (A): Cross-sectional area (cm²) |
| Compressive stress at 2.5 mm compression | kg/cm² | ( CS_{2.5} = \frac{P'}{A} ) | (P'): Load at 2.5 mm compression (kg) |
| Crushing strength at maximum load (CS at ML) | kg/cm² | ( CS_{ML} = \frac{P_o}{A} ) | (P_o): Maximum load (kg) |
| Modulus of Elasticity perpendicular to grain | kg/cm² | ( M_E = \frac{P \times h}{A \times \Delta} ) | (h): Specimen height (cm), (\Delta): Deformation at LP (cm) |
| Characteristic | Unit | Formula | Notes |
|---|---|---|---|
| Fibre stress at LP (FS at LP) | kg/cm² | ( FS_{LP} = \frac{3P a}{b h^2} ) | (a): Load to support distance (cm), (b): breadth (cm), (h): depth (cm) |
| Equivalent fibre stress at max load (Modulus of Rupture) | kg/cm² | ( M_R = \frac{3P' a}{b h^2} ) | (P'): Max load (kg) |
| Modulus of elasticity | kg/cm² | ( M_E = \frac{3P a l^2}{4 b h^3 \Delta} ) | (l): gauge length (cm), (\Delta): deflection at LP (cm) |
| Horizontal shear stress at LP (ends only) | kg/cm² | ( HS_{LP} = \frac{3P |
| Characteristic | Unit | Formula |
|---|---|---|
| Tensile stress at proportional limit (TS at PL) | kg/cm² | ( \frac{P}{A} ) |
| Tensile stress at maximum load (TS at ML) | kg/cm² | ( \frac{P'}{A} ) |
| Modulus of elasticity in tension (M of E) | kg/cm² | ( \frac{L P}{A \Delta} ) |
| Characteristic | Unit | Formula |
|---|---|---|
| Fibre stress at limit of proportionality (FS at LP) | kg/cm² | ( \frac{3 P l}{2 b h^2} ) |
| Equivalent fibre stress at max load (Modulus of Rupture, M of R) | kg/cm² | ( \frac{3 P' l}{2 b h^2} ) |
| Modulus of elasticity (M of E) | kg/cm² | ( \frac{P l^3}{4 b h^3 \Delta} ) |
| Characteristic | Unit | Formula |
|---|---|---|
| Horizontal shear stress at PL (ends) | kg |
| Test Type | Specimen Size (cm) | Failure Plane | Key Formula | Units |
|---|---|---|---|---|
| Shear Strength | 5x5x6 or 2x2x3 | Radial/Tangential | ( MSS = \frac{P_{max}}{A} ) | kg/cm² or N/mm² |
| Cleavage Strength | As per drilled holes | Radial/Tangential | ( \frac{P_{max}}{b} ) | kg/cm |
flowchart LR
A[Specimen Preparation] --> B[Notching / Drilled Holes]
B --> C[Setup on Testing Rig]
C --> D{Apply Load
IS 1708 Part 10: Hardness Testing of Timber (Static Indentation)
| Characteristic | Unit | Formula | Variables Description |
|---|---|---|---|
| Maximum height of drop (H) | cm | H | Maximum drop height under given weight |
| Height of drop at limit of proportionality (H') | cm | H' | Drop height at proportionality limit from curve |
| Fibre stress at limit of proportionality (FS) | kg/cm² | (\displaystyle FS = \frac{3 H' W I}{b h^2 4}) | (W)=weight (kg), (I)=span (cm), (b)=breadth (cm), (h)=depth (cm), (4 = (x+y)) deflection at LP |
| Modulus of Elasticity (M of E) | kg/cm² | (\displaystyle M = \frac{H' W I^3}{2 b h^3 42}) | Same variables as above |
| Work to limit of proportionality | kg cm/cm³ | (\displaystyle Work = \frac{H' W I}{b h}) | Same variables as above |
flowchart LR
A[Steel Ball (Ø 1.128 cm)] --> B[Indentation on Timber Surface]
B -->
Nail and Screw Holding Power
As per IS 1708 (Part 15 & 16) - 1986
[ P = F_{max} ]
Where:
| Condition | Nail Holding Power (N) | Screw Holding Power (N) |
|---|---|---|
| Green timber, immediate pull | 1500 - 2000 | 2000 - 2500 |
| Green timber, after drying | 1800 - 2200 | 2200 - 2700 |
| Dry timber (12% moisture) | 2000 - 2500 | 2500 - 3000 |
flowchart LR
A[Test Specimen Preparation] --> B[Nail/Screw Driven]
B --> C[Specimen Mounted on Testing Machine]
C --> D[Load Applied to Pull Out Nail/Screw]
D --> E[Max Load Recorded for Radial, Tangential, End Surfaces
IS 1708 Part 16-18: Brittleness Testing (Charpy & Izod Impact)
| Test Type | Cross-section (mm) | Length (mm) | Notch Details (Charpy) |
|---|---|---|---|
| Izod | 10 (point of impact) | As per Fig.1 | - |
| Charpy | 12.5 x 12.5 | 125 | V-notch: 2.5 mm depth, 5 mm width at radial face |
| No. | Characteristic | Unit | Formula | Notes |
|---|---|---|---|---|
| 1 | Fibre Stress at Limit of Proportionality (FS at LP) | kg/cm² | ( FS = \frac{3P a}{b h^2} ) | P = load at LP, a = distance load-support, b = breadth, h = depth |
| 2 | Equivalent Fibre Stress at Max Load (Modulus of Rupture, MOR) | kg/cm² | ( MOR = \frac{3P' a}{b h^2} ) | P' = maximum load |
| 3 | Modulus of Elasticity (MOE) | kg/cm² | ( MOE = \frac{3P a l^2}{4 b h^3 \delta} ) | l = gauge length, δ = deflection at LP |
| 4 | Horizontal Shear Stress at LP (HS at PL) | kg/cm² | At center = 0; At ends = ( \frac{3P}{4 b h} ) | - |
| 5 | Horizontal Shear Stress at Max Load (HS at ML) | kg/cm² | At center = 0; At ends = ( \frac{3P'}{4 b h} ) | - |
| 6 | Work to Limit of Proportionality (Elastic Resilience) | kg.cm/cm³ | ( Wk = \frac{P \Delta^2 l}{2 b h} ) | Δ = deflection at LP, l = gauge length |
IS 1708 Part 18 - Torsional Strength Testing of Timber: Key Points
[ \tau = \frac{T \cdot r}{J} ]
Where:
(T) = Applied torque (N·mm)
(r) = Radius of specimen (mm)
(J = \frac{\pi r^4}{2}) = Polar moment of inertia for circular section (mm⁴)
Angle of twist, θ:
[ \theta = \frac{T \cdot L}{G \cdot J} ]
Where:
| Parameter | Formula | Units |
|---|---|---|
| Polar moment of inertia (J) | ( \frac{\pi r^4}{2} ) | mm⁴ |
| Torsional shear stress (τ) | ( \frac{T \cdot r}{J} ) | N/mm² |
| Angle of twist (θ) | ( \frac{T \cdot L}{G \cdot J} ) | radians |
Moisture Content Control and Conditioning (IS 1708 Part 1-18)
Moisture Content (%)
[
\text{Moisture Content} = \frac{W_1 - W_0}{W_0} \times 100
]
Where:
Volumetric Shrinkage
[
\text{Volumetric Shrinkage} = \frac{V_1 - V_T}{V_1} \times 100
]
Where:
| Parameter | Symbol | Unit | Condition/Notes |
|---|---|---|---|
| Weight at test | (W_1) | g | At current moisture content |
| Oven dry weight | (W_0) | g | After oven drying |
| Initial volume | (V_1) | cc | Green (wet) condition |
| Volume at dry state | (V_T) | cc | At required dry moisture |
| Target moisture content | — | % | ~12% for testing |
flowchart LR
A[Green Specimen] -->|Measure W1, V1| B[Calculate Moisture Content]
B --> C{Moisture Content > 12%?}
C -- Yes --> D[Air Seasoning & Periodic Weighing]
D --> B
C -- No --> E[Specimen Ready for Testing]
This ensures consistent moisture content for reliable timber testing as per IS 1708.
Frequently Asked
IS 1708 Part 1-18: Test Specimen Dimensions & Preparation
Dimensions:
Preparation:
| Cross-section (cm) | Length (cm) | Notes |
|---|---|---|
| 5 x 5 | 6, 15, 20, 100 | Defect-free, grain slope ≤1/20 |
| 2 x 2 | 3, 8, 15, 20, 40 | Can be glued for larger cross-section |
This ensures consistent, reliable test results per IS 1708 standards.
According to IS 1708 (Part 2), the specific gravity of timber is determined as follows:
[ \text{SG}_{test} = \frac{W_1}{V_1} ]
[ \text{SG}_{adjusted} = \frac{W_1}{V_1} \times \frac{100}{100 + m} ]
Where:
[ \text{SG}_{oven-dry} = \frac{W_0}{V_0} ]
Where:
Note:
This method ensures consistent timber density measurement accounting for moisture variations.
Standard Loading Rates for Static and Impact Bending Tests (IS 1708 Parts 1-18):
For static bending tests, the load application rate depends on specimen size:
For impact bending tests, the code typically specifies a rapid load application, but exact rates are not detailed in the provided context. Impact tests rely on drop weight or pendulum impact devices, where energy and velocity are controlled rather than displacement rate.
| Test Type | Specimen Size (cm) | Loading Rate (mm/min) |
|---|---|---|
| Static Bending | 5 × 5 × 75 | 2.5 – 3.0 |
| Static Bending | 2 × 2 × 30 | 0.6 – 1.5 |
| Impact Bending | N/A | Rapid (velocity controlled) |
Note: Always refer to the specific Part of IS 1708 relevant to your material for exact rates.
IS 1708 (Part 15 & 16) - Nail and Screw Holding Power
Definition: Holding power is the maximum load required to pull out nails or screws from timber.
Test Specimen:
Test Setup:
Measurement:
Conditions Tested:
Loading diagram...
This method ensures standardized evaluation of fastener holding strength in timber.
Moisture Content Control Procedures (IS 1708 Part 1-18):
Specimen Sampling (Clause 2.1):
Prevent Moisture Change (Clause 3.2):
Conditioning (Clause 3.3):
| Step | Action |
|---|---|
| Sampling | Cut immediately after test, near failure point |
| Initial Handling | Wipe dry, coat ends with hot paraffin |
| Conditioning | Air-season at room temp, weigh periodically |
| Target Moisture Content | Approximately 12% uniform moisture |
Loading diagram...
This ensures accurate moisture content measurement critical for reliable mechanical property evaluation.
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