IS 1708 Part 1-181986AI Search Enabled✦ AI Generated

Methods of testing of small transparent specimens of timber

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.

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What This Standard Covers

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.

Who Uses This Standard

  • Structural Engineers
  • Wood Scientists and Researchers
  • Quality Control Inspectors in Timber Industry
  • Civil Engineers
  • Material Testing Laboratories
  • Forest Product Manufacturers
  • Timber Design Consultants

Key Topics Covered

Preparation and dimensions of test specimens
Determination of specific gravity of timber
Static bending strength under two-point and central loading
Impact bending strength and brittleness testing
Compressive strength parallel and perpendicular to grain
Tensile strength parallel and perpendicular to grain
Shear strength and cleavage strength parallel to grain
Hardness testing by static indentation
Nail and screw holding power evaluation
Torsional shear strength measurement
Moisture content control and specimen conditioning
Load application rates and measurement techniques

Table of Contents

1Scope

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.


Key Formulas (Clause 4.2 & 4.3)

CharacteristicUnitFormulaNotes
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/cm²At ends: ( \frac{3P}{4 b h} ), Center: 0
Horizontal shear stress at max loadkg/cm²At 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} )

Impact Test Related (Clause 4.3)

CharacteristicUnitFormula
Maximum height of drop (H)cmMeasured directly
Height of drop at LP (H')cmFrom 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
2Test Specimen Preparation and Dimensions

IS 1708 Part 1-18: Test Specimen Preparation and Dimensions

Specimen Sizes & Shapes (Clause 2.1)

  • Two specimen sizes:
    • Size 1: 5 × 5 cm cross-section, length 20 cm (or 6 cm for shear test)
    • Size 2: 2 × 2 cm cross-section, length 8 cm (or 3 cm for shear test)

Notch and Failure Area

  • Notches as per Fig. 1A & 1B to induce failure in radial or tangential surface.
  • Failure area:
    • 50 × 20 mm (for 5 × 5 cm specimen)
    • 20 × 10 mm (for 2 × 2 cm specimen)

Additional Specifications

  • Specimens must be free of defects.
  • Grain slope ≤ 1:20 relative to longitudinal edges.
  • End planes must be perpendicular to specimen length.
  • Notches are designed to produce shear failure on specified surface areas.

Summary Table

Specimen SizeCross-Section (cm)Length (cm)Failure Area (mm)Failure Plane
Large5 × 520 (6 shear)50 × 20Radial or Tangential
Small2 × 28 (3 shear)20 × 10Radial or Tangential

This ensures standardized specimen preparation for consistent shear testing results.

3Test Procedures and Loading Rates

IS 1708 Part 1-18: Test Procedures & Loading Rates

Key Specifications for Rate of Loading (Clause 3.2):

  • The movable head of the testing machine must move at a constant rate during the test.
  • Typical rates specified:
    • 2.5 mm/min until maximum load (for both sizes).
    • Alternative rates mentioned: 0.4 mm/min and 0.6 mm/min (context-dependent).

Summary Table of Loading Rates:

Test Size/TypeRate of Movable Head (mm/min)Notes
Both sizes2.5Continuous loading until max load
Both sizes0.6Alternative rate
Both sizes0.4Alternative rate

Important Notes:

  • The load must be applied continuously and smoothly to avoid shock loading.
  • The rate ensures uniform stress application and accurate measurement of strength.
  • Data recording should be synchronized with the displacement and load to capture peak values.
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.

4Recording of Data and Calculations

IS 1708 Part 1-18: Recording of Data and Calculations

Key Specifications:

  • Loading rate: 6 mm/min constant travel of machine head (Clause 3.2).
  • Failure recording: According to appearance/development per Fig. 2 (Clause 3.4).

Important Formulas (Clause 4.2):

CharacteristicUnitFormula
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 workkg·cm/cm³( \frac{C A''}{l b h} )

Parameters:

  • (P) = Load at limit of proportionality (kg)
  • (P') = Maximum load (kg)
  • (l) = Span length (cm)
  • (b) = Breadth of specimen (cm)
  • (h) = Depth of specimen (cm)
  • (\Delta) = Deflection at load (P) (cm)
  • (C) = Area constant (kg·cm)
  • (A, A', A'') = Areas under load-deflection curve up to LP, max load, and final
5Specific Gravity Determination

Specific Gravity Determination (IS 1708 Part 1-18)

Key Formulas:

  1. Specific Gravity at Test Condition: [ \text{Specific Gravity} = \frac{W_1}{V_1} ]

    • (W_1) = weight of test specimen (g)
    • (V_1) = volume of test specimen (cm³)
  2. Adjusted Specific Gravity (considering moisture content): [ \text{Adjusted Specific Gravity} = \frac{W_1}{V_1} \times \frac{100}{100 + m} ]

    • (m) = moisture content (%) of specimen
  3. Oven Dry Specific Gravity: [ \text{Oven Dry Specific Gravity} = \frac{W_o}{V_o} ]

    • (W_o) = oven dry weight (g)
    • (V_o) = oven dry volume (cm³)

Specimen Dimensions (Clause 2.2):

  • For specific gravity test:
    • Cross-section: 5 x 5 cm, Length: 15 cm
    • Or Cross-section: 2 x 2 cm, Length: 6 cm
    • If rectangular specimens unavailable: volume ≈ 10 cm³

Notes:

  • Standard Specific Gravity: Adjusted specific gravity for green specimens (above fibre saturation point).
  • Dry Specific Gravity: Specific gravity of dry specimens.

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[
6Static Bending Strength Tests

IS 1708 Part 1-18: Static Bending Strength Tests Summary


Specimen Dimensions (Clause 2.1)

  • 5 x 5 cm cross-section, 75 cm length, or
  • 2 x 2 cm cross-section, 30 cm length
  • Grain slope ≤ 1:20, defect-free specimens.

Key Formulas (Clause 4.2)

CharacteristicFormulaUnits
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
  • P = load at limit of proportionality (kg)
  • P' = maximum load (kg)
  • l = span length (cm)
  • b = breadth (cm)
  • h = depth (cm)
  • δ = deflection at P (cm)
  • C = energy per unit area under load-deflection curve (kg·cm)
7Impact Bending Strength Tests

Impact Bending Strength Test (IS 1708 Part 1-18)

Specimen Dimensions (Clause 2.1)

  • Size 1: 5 × 5 cm cross-section, 75 cm length
  • Size 2: 2 × 2 cm cross-section, 30 cm length
  • Grain slope ≤ 1:20 parallel to edges.

Test Setup (Clause 3.1)

  • Span:
    • 70 cm for 5 × 5 × 75 cm
    • 28 cm for 2 × 2 × 30 cm
  • Hammer weight:
    • 25 kg (large specimen)
    • 1.5 kg (small specimen)
  • Hammer face radius: 75 cm (large), 30 mm (small).
  • Impact on tangential surface near heartwood.
  • For stronger species, double hammer weight and height.

Key Formulas (Clause 4.2)

CharacteristicFormulaUnit
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:

  • ( P ) = load at limit of
8Compressive Strength Tests

Key Formulas for Compressive Strength Tests (IS 1708 Parts 1-18)

1. Compressive Stress Calculations (Clause 4.1)

CharacteristicUnitFormulaDescription
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 compressionkg/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 grainkg/cm²( M_E = \frac{P \times h}{A \times \Delta} )(h): Specimen height (cm), (\Delta): Deformation at LP (cm)

2. Compression Parallel to Grain (Clause 4.2)

CharacteristicUnitFormulaNotes
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 elasticitykg/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
9Tensile Strength Tests

Key Formulas & Specifications for Tensile Strength Tests (IS 1708 Parts 1-18)


1. Tensile Strength Parallel to Grain (IS 1708 Part 12)

CharacteristicUnitFormula
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} )
  • P = Load at proportional limit (kg)
  • P' = Maximum load (kg)
  • A = Cross-sectional area (cm²)
  • L = Gauge length between extensometer points (cm)
  • Δ = Elongation at proportional limit (cm)

2. Tensile Strength Perpendicular to Grain (IS 1708 Part 13)

CharacteristicUnitFormula
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} )
  • P, P' = Load at proportional limit, max load (kg)
  • l = Span length (cm)
  • b = Breadth (cm)
  • h = Depth (cm)
  • Δ = Deflection at proportional limit (cm)

3. Horizontal Shear Stress (IS 1708 Part 5 & 6)

CharacteristicUnitFormula
Horizontal shear stress at PL (ends)kg
10Shear and Cleavage Strength Tests

Shear and Cleavage Strength Tests as per IS 1708 (Parts 1-18)


1. Shear Strength Test (IS 1708 Part 15 & 11)

  • Specimen size:
    • 5 x 5 cm cross-section, 6 cm length or
    • 2 x 2 cm cross-section, 3 cm length.
  • Notching: On one end to induce shear failure on radial or tangential plane.
  • Test Setup:
    • Specimen supported by cross bar with edges vertical.
    • Shearing tool rests on the notch.
    • Shearing direction parallel to grain.
  • Formula for Maximum Shearing Stress (MSS):
    [ MSS = \frac{P_{max}}{A} ]
    Where:
    (P_{max}) = Maximum load at failure (kg or N)
    (A) = Shear area (cm² or mm²)

2. Cleavage Strength Test (IS 1708 Part 14)

  • Specimen: With drilled holes (Ø 4 mm) as per Fig. 1.
  • Formula for Cleavage Resistance:
    [ \text{Cleavage Resistance (kg/cm)} = \frac{P_{max}}{b} ]
    Where:
    (P_{max}) = Maximum load at failure (kg or N)
    (b) = Width of the specimen (cm)

Summary Table

Test TypeSpecimen Size (cm)Failure PlaneKey FormulaUnits
Shear Strength5x5x6 or 2x2x3Radial/Tangential( MSS = \frac{P_{max}}{A} )kg/cm² or N/mm²
Cleavage StrengthAs per drilled holesRadial/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
11Hardness Testing

IS 1708 Part 10: Hardness Testing of Timber (Static Indentation)

Key Specifications:

  • Indentation Tool: Steel ball or hemispherical steel bar, diameter = 1.128 cm.
  • Indentation Depth: Standard depth = 0.564 cm.
  • Load: Load in kg required to penetrate to the specified depth is recorded.
  • Surfaces Tested: Tangential, radial, and end surfaces.
  • Hardness Values:
    • Average of two penetrations on one surface or one penetration on both ends.
    • Side hardness = average of radial and tangential hardness.

Important Formulae (Clause 4.3):

CharacteristicUnitFormulaVariables Description
Maximum height of drop (H)cmHMaximum drop height under given weight
Height of drop at limit of proportionality (H')cmH'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 proportionalitykg cm/cm³(\displaystyle Work = \frac{H' W I}{b h})Same variables as above

Notes:

  • For compressive stress perpendicular to grain, ratio of results for 5x5 cm and 2x2 cm cross-sections = 1.07 (Clause 5.1).
  • Hardness is evaluated by static indentation load required for standard penetration.

Summary Diagram of Hardness Test Setup:

flowchart LR
    A[Steel Ball (Ø 1.128 cm)] --> B[Indentation on Timber Surface]
    B -->
12Nail and Screw Holding Power

Nail and Screw Holding Power
As per IS 1708 (Part 15 & 16) - 1986


Nail Specifications (Clause 3.2, Part 15)

  • Length: 50 mm
  • Shank Diameter: 2.50 mm
  • Type: Bright, galvanized, diamond pointed, plain heads
  • Usage: Each nail used only once

Test Specimen & Setup (Clause 1.1 & 4.1)

  • Specimen prepared per IS 1708 Part 15
  • Testing machine grips timber fixed head & nail/screw movable head
  • Load applied to pull out nail/screw recorded

Data Recording (Clause 4.3)

  • Record max load to pull out nails/screws on:
    • Radial surface
    • Tangential surface
    • End surface
  • Average of radial & tangential = Side value

Test Conditions (Note, Clause 4.3)

  • Nails/screws driven in:
    1. Green timber, pulled immediately
    2. Green timber, pulled after drying to 12% moisture
    3. Dry timber (12% moisture), pulled immediately

Typical Holding Power Formula (General Engineering Knowledge)

[ P = F_{max} ]

Where:

  • (P) = Nail/Screw holding power (N)
  • (F_{max}) = Maximum pull-out load recorded (N)

Summary Table (Example)

ConditionNail Holding Power (N)Screw Holding Power (N)
Green timber, immediate pull1500 - 20002000 - 2500
Green timber, after drying1800 - 22002200 - 2700
Dry timber (12% moisture)2000 - 25002500 - 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
13Brittleness Testing

IS 1708 Part 16-18: Brittleness Testing (Charpy & Izod Impact)


Specimen Dimensions:

Test TypeCross-section (mm)Length (mm)Notch Details (Charpy)
Izod10 (point of impact)As per Fig.1-
Charpy12.5 x 12.5125V-notch: 2.5 mm depth, 5 mm width at radial face

Key Formulas (Clause 4.2):

No.CharacteristicUnitFormulaNotes
1Fibre 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
2Equivalent Fibre Stress at Max Load (Modulus of Rupture, MOR)kg/cm²( MOR = \frac{3P' a}{b h^2} )P' = maximum load
3Modulus of Elasticity (MOE)kg/cm²( MOE = \frac{3P a l^2}{4 b h^3 \delta} )l = gauge length, δ = deflection at LP
4Horizontal Shear Stress at LP (HS at PL)kg/cm²At center = 0; At ends = ( \frac{3P}{4 b h} )-
5Horizontal Shear Stress at Max Load (HS at ML)kg/cm²At center = 0; At ends = ( \frac{3P'}{4 b h} )-
6Work 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

Notes:

  • P =
14Torsional Strength Testing

IS 1708 Part 18 - Torsional Strength Testing of Timber: Key Points

1. Specimen Dimensions (Clause 2.1 & Fig. 1)

  • Shape: Cylindrical
  • Central length: 220 mm
  • Radius:
    • Large size: 25 mm
    • Small size: 12 mm
  • End portions for gripping:
    • Length: 40 mm
    • Large size: 30 mm radius
    • Small size: 15 mm radius

2. Test Setup (Clause 3.1)

  • Specimen fixed firmly at one end.
  • Free to rotate at the other.
  • Angular twist measured at the center over a gauge length of 150 mm.

3. Calculation of Torsional Shear Stress and Modulus

  • Torsional shear stress, τ:

[ \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:

  • (L) = Gauge length (mm)
  • (G) = Modulus of rigidity (shear modulus) (N/mm²)

4. Data Interpretation (Clause 4.1)

  • Plot Torque vs Angular Twist curve.
  • Determine proportional limit and maximum load.
  • Calculate shear strength at proportional limit and maximum load.

Summary Table of Formulas

ParameterFormulaUnits
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
15Moisture Content Control and Conditioning

Moisture Content Control and Conditioning (IS 1708 Part 1-18)

Key Formulas:

  • Moisture Content (%)
    [ \text{Moisture Content} = \frac{W_1 - W_0}{W_0} \times 100 ]
    Where:

    • (W_1) = weight of sample at test (g)
    • (W_0) = oven-dry weight of sample (g)
  • Volumetric Shrinkage
    [ \text{Volumetric Shrinkage} = \frac{V_1 - V_T}{V_1} \times 100 ]
    Where:

    • (V_1) = volume at initial (green) condition (cc)
    • (V_T) = volume at dry condition (cc)

Conditioning Specifications:

  • Specimens must be air-seasoned until moisture content reaches approximately 12%.
  • Weigh and measure specimens periodically with accuracy as per Clause 3.1.
  • Oven-dry condition is considered the reference for zero moisture content.

Summary Table:

ParameterSymbolUnitCondition/Notes
Weight at test(W_1)gAt current moisture content
Oven dry weight(W_0)gAfter oven drying
Initial volume(V_1)ccGreen (wet) condition
Volume at dry state(V_T)ccAt 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.

Popular Questions About IS 1708 Part 1-18

?What are the specified dimensions and preparation methods for test specimens?

IS 1708 Part 1-18: Test Specimen Dimensions & Preparation

  • Dimensions:

    • Cross-section options:
      • 5 x 5 cm with lengths of 6 cm, 15 cm, 20 cm, or 100 cm depending on test type.
      • 2 x 2 cm with lengths of 3 cm, 8 cm, 15 cm, 20 cm, 40 cm depending on test.
    • If 5 x 5 cm not available, glue 2 x 2 cm sticks to form at least 4 x 4 cm cross-section with aligned grain.
  • Preparation:

    • Specimens must be defect-free.
    • Slope of grain ≤ 1 in 20 parallel to longitudinal edges.
    • End planes must be perpendicular to specimen length.
    • For shear tests, specimens are notched at one end (see Fig. 1 in code) to induce shear failure on 5 x 5 cm or 2 x 2 cm surface in radial/tangential plane.

Summary Table

Cross-section (cm)Length (cm)Notes
5 x 56, 15, 20, 100Defect-free, grain slope ≤1/20
2 x 23, 8, 15, 20, 40Can be glued for larger cross-section

This ensures consistent, reliable test results per IS 1708 standards.

?How is the specific gravity of timber determined according to IS 1708?

According to IS 1708 (Part 2), the specific gravity of timber is determined as follows:

1. Test Specimen Preparation

  • Measure weight (W1) in grams.
  • Measure volume (V1) in cm³.
  • Determine moisture content (m) (%) as per Part 1.

2. Specific Gravity Calculation

  • Specific gravity at test condition:

[ \text{SG}_{test} = \frac{W_1}{V_1} ]

  • Adjusted (standard) specific gravity:

[ \text{SG}_{adjusted} = \frac{W_1}{V_1} \times \frac{100}{100 + m} ]

Where:

  • ( W_1 ) = weight of specimen (g)
  • ( V_1 ) = volume of specimen (cm³)
  • ( m ) = moisture content (%)

3. Oven-Dry Specific Gravity (from Part 1, Clause 4.2)

[ \text{SG}_{oven-dry} = \frac{W_0}{V_0} ]

Where:

  • ( W_0 ) = oven-dry weight (g)
  • ( V_0 ) = oven-dry volume (cm³)

Note:

  • If specimen is green (above fibre saturation), adjusted SG = standard specific gravity.
  • If specimen is oven-dry, SG = dry specific gravity.

This method ensures consistent timber density measurement accounting for moisture variations.

?What are the standard loading rates for static and impact bending tests?

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:

    • 5 × 5 × 75 cm specimens: movable head speed = 2.5 mm/min (Part 1)
    • 2 × 2 × 30 cm specimens: movable head speed = 1.0 mm/min (Part 1)
    • Alternative rates (Part 5):
      • Larger specimens: 3 mm/min
      • Smaller specimens: 1.5 mm/min
    • For some parts (e.g., Part 6), a uniform rate of 0.6 mm/min is specified regardless of 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.


Summary Table:

Test TypeSpecimen Size (cm)Loading Rate (mm/min)
Static Bending5 × 5 × 752.5 – 3.0
Static Bending2 × 2 × 300.6 – 1.5
Impact BendingN/ARapid (velocity controlled)

Note: Always refer to the specific Part of IS 1708 relevant to your material for exact rates.

?How does the standard define and measure nail and screw holding power?

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:

    • Nail: 50 mm length, 2.50 mm shank diameter, bright galvanized, diamond pointed, plain head (Clause 3.2).
    • Screws as per Part 15 specifications.
  • Test Setup:

    • Specimen gripped firmly; nail/screw held by movable head on a testing machine (Clause 4.1).
    • Load applied until nail/screw is pulled out.
  • Measurement:

    • Record maximum pull-out load for three grain directions: radial, tangential, and end grain.
    • Average of radial and tangential values = side holding power (Clause 4.3).
  • Conditions Tested:

    • Nails/screws driven in green wood, pulled immediately.
    • Driven in green wood, pulled after drying to 12% moisture.
    • Driven in dry wood (12% moisture), pulled immediately.
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This method ensures standardized evaluation of fastener holding strength in timber.

?What procedures are recommended for controlling moisture content during testing?

Moisture Content Control Procedures (IS 1708 Part 1-18):

  • Specimen Sampling (Clause 2.1):

    • Take specimens immediately after mechanical testing, near failure point.
    • Size: ~2.5 cm length, full cross-section (5x5 cm or 2x2 cm for shear tests).
    • For moisture-only tests, use 2.5 cm length × 2x2 cm or 5x5 cm cross-section.
  • Prevent Moisture Change (Clause 3.2):

    • Avoid moisture change between cutting and first weighing.
    • After water removal, wipe dry, end-coat with hot paraffin to seal, preventing moisture loss/gain.
    • Air-season specimens at room temperature.
  • Conditioning (Clause 3.3):

    • Air-season specimens, periodically weigh and measure until uniform moisture content ~12% is reached.

Summary Table:

StepAction
SamplingCut immediately after test, near failure point
Initial HandlingWipe dry, coat ends with hot paraffin
ConditioningAir-season at room temp, weigh periodically
Target Moisture ContentApproximately 12% uniform moisture
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This ensures accurate moisture content measurement critical for reliable mechanical property evaluation.

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