IS 13946 Part 21994AI Search Enabled✦ AI Generated

Determination of rock stress-Code of practice, Part 2: Using USBM-type drill hole deformation gauge

IS 13946 Part 2 (1994) provides a code of practice for determining in situ rock stresses using the USBM-type drillhole deformation gauge method. It guides engineers on drilling, gauge insertion, overcoring procedures, and data interpretation to measure secondary principal stresses perpendicular to the drillhole axis. This standard is essential for geotechnical engineers, mining engineers, and rock mechanics professionals involved in underground excavation design, rock stability analysis, and stress evaluation in rock masses.

9Sections
48Clauses Indexed
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1994Edition
Rock MechanicsCategory
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What This Standard Covers

IS 13946 Part 2 (1994) provides a code of practice for determining in situ rock stresses using the USBM-type drillhole deformation gauge method. It guides engineers on drilling, gauge insertion, overcoring procedures, and data interpretation to measure secondary principal stresses perpendicular to the drillhole axis. This standard is essential for geotechnical engineers, mining engineers, and rock mechanics professionals involved in underground excavation design, rock stability analysis, and stress evaluation in rock masses.

Who Uses This Standard

  • Geotechnical Engineers
  • Mining Engineers
  • Rock Mechanics Specialists
  • Civil Engineers involved in underground construction
  • Geologists
  • Hydrogeologists
  • Research Scientists in rock mechanics

Key Topics Covered

USBM-type drillhole deformation gauge principles
Drilling and overcoring procedures
Pilot hole and overcore hole specifications
Gauge calibration and insertion techniques
Measurement of drillhole diameter deformation
Calculation of secondary principal stresses
Determination of Young's modulus and Poisson's ratio
Data recording and field data sheets
Biaxial modulus chamber testing
Interpretation of stress components and orientations
Handling anisotropic rock conditions
Reporting requirements for stress measurement
Drillhole configuration and site selection
Equipment specifications for stress testing
Statistical treatment of stress data

Table of Contents

1Scope

Scope & Key Specifications from IS 13946 Part 2 (1994):

  • Purpose: Measurement of in-situ rock stresses by overcoring method using deformation gauges.

Key Report Contents (Clause 7.1 & 7.2)

  • General Info: Drillhole location, direction, length; geotechnical core log; equipment & procedure description with diagrams/photos.
  • Detailed Data:
    • Field data sheets or plots showing overcoring deformation (Fig. 3).
    • Estimated principal strains: U1, U2, U3.
    • Radial pressure vs borehole deformation or stress-strain curves.
    • Tabulation of hole number, bearing, inclination, depth, Young’s modulus, Poisson’s ratio.
    • Principal stress magnitudes, directions, and statistical parameters.
    • Explanation of discrepancies in test results.

Equipment Requirements (Clauses 4.2 & 4.3)

  • Deformation Gauge:
    • Measures pilot hole diameter changes in 1-3 orientations.
    • Sensitivity: Detect changes as small as 1 part in 10.
    • Must be waterproof, firmly held, detachable from cable.
    • Example: USBM gauge with strain gauges on cantilever arms.
  • Others:
    • Strain indicator readout bridge and switchgear.
    • Placement rods marked for depth and orientation.
    • Calibration device for gauge sensors.
    • Biaxial modulus chamber for Young’s modulus measurement.

Typical Plot (Fig. 3)

  • X-axis: Overcoring depth (mm)
  • Y-axis: Diameter deformation (mm)
  • Multiple curves representing deformation in different measurement planes.

Summary Table of Principal Outputs

ParameterDescription
U1, U2, U3Principal strains from overcoring
Young’s Modulus (E)From biaxial modulus chamber tests
Poisson’s Ratio (ν)From lab tests on rock cores
Principal StressesMagnitudes & directions from data

flowchart TD
    A[Drillhole Preparation] --> B[Insert Deformation Gauge]
    B --> C[Overcoring & Data Acquisition]
    C --> D[Measure Diameter Changes (U1,U2,U3
2References

IS 13946 Part 2 Key Formulas & Specifications for Overcoring Stress Measurement


1. Stress-Deformation Relationship (Plane Strain Isotropic Elasticity)

[ U = d(1 - \nu^2) \frac{1}{E} \left[ (P + Q) + 2(P - Q) \cos 2\theta \right] ]

  • ( U ): Strain in axial direction along drillhole
  • ( d ): Diameter of pilot hole
  • ( E ): Young's modulus
  • ( \nu ): Poisson's ratio
  • ( P, Q ): Major and minor secondary principal stresses
  • ( \theta ): Angle between ( P ) and measured deformation direction

2. Young's Modulus from Biaxial Chamber Test

[ E = \frac{D^2 - d^2}{2dP} U ]

  • ( D ): Diameter of overcore
  • ( d ): Diameter of pilot hole
  • ( P ): Applied radial pressure
  • ( U ): Measured change in pilot hole diameter

3. Principal Stresses & Orientation from USBM-type Gauge (3 sensors at 60°)

[ P = \frac{E}{6d} (U_1 + U_2 + U_3) + \frac{E}{2d} \sqrt{(U_1 - U_2)^2 + (U_2 - U_3)^2 + (U_3 - U_1)^2} ]

[ \theta_p = \frac{1}{2} \tan^{-1} \left[ \frac{\sqrt{3} (U_2 - U_3)}{2U_1 - U_2 - U_3} \right] ]

  • ( U_1, U_2, U_3 ): Diameter changes measured by sensors
  • ( \theta_p ): Angle of major principal stress from ( U_1 )

4. Reporting Requirements (Clause 7.2)

  • Field data sheets with ( U_1, U_2, U_3 ) values
  • Plots of radial pressure vs borehole deformation
  • Tabulation of hole number, inclination, depth, Young's modulus, Poisson's ratio
  • Stress
3Definitions

Key Definitions & Formulas from IS 13946 Part 2 (1994)

1. Diameteral Deformation (U) in Zero Axial Stress Condition (Clause 6.2):

[ U(\theta) = (P + Q) + 2(P - Q) \cos 2\theta ]

  • (P, Q): Major and minor secondary principal stresses (perpendicular to hole axis)
  • (d): Diameter of pilot hole
  • (\theta): Angle between (P) and measured deformation (U)

For USBM-type gauges with three sensors (U_1, U_2, U_3) spaced 60° apart:

[ P = \frac{E}{6d} \left(U_1 + U_2 + U_3 + 2 \sqrt{(U_1 - U_2)^2 + (U_2 - U_3)^2 + (U_3 - U_1)^2} \right) ]

[ Q = \frac{E}{6d} \left(U_1 + U_2 + U_3 - 2 \sqrt{(U_1 - U_2)^2 + (U_2 - U_3)^2 + (U_3 - U_1)^2} \right) ]

Orientation angle (\theta_p):

[ \theta_p = \frac{1}{2} \tan^{-1} \left(\frac{\sqrt{3}(U_2 - U_3)}{2U_1 - U_2 - U_3}\right) ]

Ranges for (\theta_p) depend on relative magnitudes of (U_i).


2. Young's Modulus from Biaxial Chamber (Clause 4.3 & 6.3):

[ E = \frac{D^2 - d^2}{2 d P} \times \frac{\Delta d}{d} ]

  • (D): Diameter of overcore
  • (d): Diameter of pilot hole
  • (P): Applied radial pressure
  • (\Delta d): Change in pilot hole diameter

3. 3D Case with Axial Strain (Clause 6.3):

[ U = d (1 - \nu^2

4Equipment

IS 13946 Part 2: Equipment for Overcoring Stress Measurements

Key Equipment (Clause 4.3 & 4.2)

  • Calibration device: For periodic calibration of gauge sensors to ensure accuracy.
  • Biaxial modulus chamber: Includes pressure gauge and hand pump to measure Young's modulus of large diameter cores.
  • Deformation gauge: Measures pilot hole diameter changes (usually 3 orientations). Detects changes as small as 1 part in 10. Must be waterproof, slip-resistant, and detachable from signal cable (e.g., USBM gauge with strain gauges).
  • Strain indicator readout bridge and switchgear: For signal processing.
  • Placement rods: Marked for depth and orientation to position deformation gauge inside pilot hole.

Measurement & Reporting (Clause 7.2)

Reports must include:

  • Field data sheets or plots of overcoring data (U1, U2, U3 values).
  • Radial pressure vs borehole deformation plots or stress/strain curves.
  • Tabulation of hole details, stress orientations, Young's modulus, and Poisson's ratio.
  • Principal stress magnitudes, directions, and statistical data (standard deviation, error, correlation).
  • Explanation of discrepancies with other data.

Typical Formula for Young's Modulus from Biaxial Modulus Chamber Tests:

[ E = \frac{\sigma}{\epsilon} ] Where:

  • (E) = Young's modulus
  • (\sigma) = Applied radial pressure
  • (\epsilon) = Measured strain (deformation)

Illustration: Equipment Setup for Overcoring

graph TD
    A[Deformation Gauge] --> B[Placement Rods]
    B --> C[Pilot Hole]
    C --> D[Strain Indicator Readout]
    D --> E[Calibration Device]
    F[Biaxial Modulus Chamber] --> G[Pressure Gauge & Hand Pump]
    G --> H[Rock Core Sample]

Summary:

  • Use calibrated deformation gauges to measure pilot hole diameter changes.
  • Employ a biaxial modulus chamber for Young's modulus.
  • Record detailed data including stress directions, magnitudes, and mechanical properties.
  • Follow calibration and measurement protocols strictly for reliable stress analysis.
5Drilling, Gauge Insertion and Overcoring

IS 13946 Part 2: Drilling, Gauge Insertion and Overcoring Key Points

Drilling & Overcoring (Clause 55.6 & 5.2)

  • Pilot hole diameter: 38 mm, drilled with single/double-tube core barrel (~2 m length).
  • Overcoring bit diameter: ~150 mm (3-4 times pilot hole diameter).
  • Drill rods: BQ wireline rods (55.6 mm o.d., 46 mm i.d.) or equivalent with large internal diameter for gauge passage.
  • Stabilizers: Installed every ~3 m along drill string to minimize vibration.
  • Water swivel: Connects drill rods, allows signal cable passage.
  • Core retrieval tools: Core-breaking wedge, shovel, puller.

Gauge Insertion (Clause 4.2)

  • Deformation gauge: Measures pilot hole diameter changes in 3 orientations; sensitivity ~1 part in 10.
  • Gauge features: Firmly held, waterproof, detachable from signal cable.
  • Readout: Strain indicator bridge and switchgear.
  • Placement rods: Marked for depth and orientation.

Overcoring Procedure (Clause 5.2.8)

  • Chuck speed: ~120 rpm.
  • Penetration rate: ~20 mm/min.
  • Water pressure: Low but sufficient for clearing cuttings; maintain steady.
  • Data recording: Gauge readings every 10-20 mm penetration.

Typical Overcoring Setup Diagram

graph LR
  A[Drill Rig] --> B[Drill Rods with Stabilizers]
  B --> C[Pilot Hole (38 mm)]
  C --> D[Deformation Gauge Inserted]
  B --> E[Overcoring Bit (150 mm)]
  D --> F[Signal Cable to Readout]
  B --> G[Water Swivel]
  E --> H[Rock Core Extraction Tools]

This summary ensures correct gauge placement, drilling parameters, and equipment for accurate in-situ stress measurement by overcoring per IS 13946 Part 2.

6Calculation of Stresses

Key Formulas & Specifications for Calculation of Stresses (IS 13946 Part 2)


1. Two-Dimensional Case (Stress perpendicular to drillhole axis, axial stress = 0)

[ U = d \left[(P + Q) + 2(P - Q) \cos 2\theta \right] ]

  • (U): Change in pilot hole diameter at angle (\theta)
  • (d): Diameter of pilot hole
  • (P, Q): Major and minor principal stresses perpendicular to hole axis
  • (\theta): Angle between direction of (P) and (U)

2. Three Sensor Axes (USBM-type gauge, spaced 60° apart)

  • Principal stresses: [ P, Q = \frac{E}{6d}(U_1 + U_2 + U_3) \pm \frac{E}{6d} \sqrt{2(U_1^2 + U_2^2 + U_3^2) - (U_1 U_2 + U_2 U_3 + U_3 U_1)} ]
  • Orientation of (P): [ \theta_p = \frac{1}{2} \tan^{-1} \left( \frac{\sqrt{3}(U_2 - U_3)}{2U_1 - U_2 - U_3} \right) ]

3. Three-Dimensional Case (Plane strain isotropic elasticity)

[ \varepsilon = d(1 - \nu^2)/E \cdot \left[(P + Q) + 2(P - Q) \cos 2\theta\right] ]

  • (\varepsilon): Axial strain along drillhole
  • (E): Young’s modulus
  • (\nu): Poisson’s ratio
  • Iteration possible if axial stress (\sigma_2) is known: [ \varepsilon_2 = \frac{-\sigma_2 - \nu (P + Q)}{E} ]

4. Young's Modulus from Overcoring Data

[ E = \frac{D^2 (D^2 - d^2)}{2dP} U ]

  • (D\
7Reporting of Results

IS 13946 Part 2: Reporting of Results - Key Points

1. Report Content (Clause 7.1 & 7.2)

  • General Info:

    • Drillhole location, direction, and length.
    • Geotechnical core log with depth and rock characteristics.
    • Description and diagrams/photos of equipment and procedures.
  • Detailed Data per Measurement Location:

    • Field data sheets or plots (Fig. 3) showing overcoring runs with estimated strains U1, U2, U3.
    • Radial pressure vs borehole deformation plots or stress/strain curves.
    • Tabulation including:
      • Hole number, bearing, inclination, overcore depth.
      • Measured strains (U1, U2, U3), Young’s modulus (E), Poisson’s ratio (ν).
    • Secondary principal stresses magnitudes/directions with statistical data (std. dev., error, correlation).
    • Discussion on discrepancies with explanations.

2. Key Formulas (Clause 6.3)

  • Strain in axial direction:

[ \varepsilon = d(1 - \nu^2) / E \times (P + Q) + 2(P - Q) \cos 2\theta ]

  • Young's modulus from biaxial chamber test:

[ E = \frac{D^2 - d^2}{2 d P} \times U ]

Where:

  • (D) = overcore diameter
  • (d) = pilot hole diameter
  • (P) = applied radial pressure
  • (U) = measured pilot hole diameter change
  • (\nu) = Poisson’s ratio

3. Typical Plot (Fig. 3)

  • Displays diametral deformation (mm) vs overcoring depth (mm) in the plane of measurement.

flowchart TD
    A[Drillhole Data Collection] --> B[Field Data Sheets & Plots]
    B --> C[Calculate U1, U2, U3]
    C --> D[Measure E & ν from biaxial tests]
    D --> E[Tabulate Hole Info + Strains + Elastic Properties]
    E --> F[Compute Principal Stresses & Directions]
    F --> G[
Annex ATypical Field Data Sheet

Typical Field Data Sheet - Key Formulas, Tables & Specifications (IS 13946 Part 2)


1. Data to Record (Clause 7.2 & 7.1)

  • Drillhole ID, bearing, inclination, depth of overcore.
  • Measured diameter changes: U1, U2, U3 (three orthogonal directions).
  • Young’s modulus (E) and Poisson’s ratio (ν) at test location.
  • Radial pressure (P) and borehole deformation (U) from biaxial chamber tests.
  • Stress magnitudes and directions (σ1, σ2, σ3) with statistical errors.
  • Geological and structural logs of rock core.
  • Equipment and procedure details.

2. Key Formulas

  • Young’s Modulus from Biaxial Chamber Test:

[ E = \frac{D^2 - d^2}{2dP} \times U ]

Where:

  • (D) = Diameter of overcore

  • (d) = Diameter of pilot hole

  • (P) = Applied radial pressure

  • (U) = Measured change in pilot hole diameter

  • Strain in axial direction (ε):

[ \varepsilon = \frac{1}{E} \left[(1 - \nu^2)(P + Q) + 2(P - Q) \cos 2\theta \right] ]

  • Axial strain with axial stress σ2:

[ \varepsilon_2 = -\frac{\sigma_2 - \nu (P + Q)}{E} ]


3. Typical Plot (Fig. 3)

  • Plot of diametral deformation (mm) vs overcoring depth (mm) for each measurement plane.

4. Measurement Procedure (Clause 5.2.8)

  • Chuck speed: ~120 rev/min
  • Penetration rate: ~20 mm/min
  • Record gauge readings every 10-20 mm penetration
  • Maintain steady low water pressure for clearing cuttings

Mermaid Diagram: Data Flow in Field Data Sheet Preparation

flowchart LR
    A[Drillhole Info] --> B[Overcoring Measurements (U1,U2,U3)]
    B --> C[
Annex BCommittee Composition

Committee Composition - IS 13946 Part 2 (1994)

Rock Mechanics Sectional Committee, CED 48

  • Chairman: Dr. Bhawani Singh, University of Roorkee
  • Members: Experts from Irrigation Departments, CSIR Institutes, Geological Survey of India, Central Water & Power Research Station, IIT Delhi, National Thermal Power Corporation, BIS, and others.
  • Member-Secretary: Dr. R. P. Kulkarni, Central Board of Irrigation & Power

Field Testing of Rock Mass and Rock Mass Classification Subcommittee, CED 48:1

  • Convener: Shri U. S. Rajvanshi, U.P. Irrigation Research Institute
  • Members: Professors from University of Roorkee, Indian School of Mines, experts from Government Irrigation Departments, CSIR, IIT Delhi, National Hydroelectric Power Corporation, and other research institutes.

Key Specifications from IS 13946 Part 2

  • Field Data Sheet: Records hole number, date, orientation, calibration factors, deformation, temperature, water presence, and remarks.
  • Measurement Data: Includes three deformation readings (U1, U2, U3), hole orientation, depth, and Young’s modulus & Poisson’s ratio.
  • Young’s Modulus Calculation:

[ E = \frac{D^2 - d^2}{2dP} \times U ]

Where:

  • (D) = diameter of overcore

  • (d) = diameter of pilot hole

  • (P) = applied radial pressure

  • (U) = measured change in pilot hole diameter

  • Stress-Strain Relation (3D isotropic elasticity):

[ \varepsilon = d (1 - \nu^2) E (P + Q) + 2(P - Q) \cos 2\theta ]

Where:

  • (\varepsilon) = axial strain
  • (\nu) = Poisson’s ratio
  • (P, Q) = stress components
  • (\theta) = orientation angle

Summary Diagram of Committee Structure

graph TD
    A[Rock Mechanics Sectional Committee] --> B(Chairman: Dr. Bhawani Singh)
    A --> C(Members: Experts from various Govt &

Popular Questions About IS 13946 Part 2

?What is the principle behind the USBM-type drillhole deformation gauge method?

Principle of USBM-type Drillhole Deformation Gauge Method (IS 13946 Part 2):

  • The USBM gauge measures secondary principal stresses (P and Q) in the plane perpendicular to the drillhole axis by detecting changes in the pilot hole diameter during overcoring.

  • The gauge uses cantilever-mounted electric resistance strain gauges to measure diameter changes (U) at three orientations spaced 60° apart (U1, U2, U3).

  • When axial stress is zero, the diameter change at angle θ is:

    [ U(\theta) = (P + Q) + 2 (P - Q) \cos 2\theta ]

  • Using the three measured deformations, principal stresses and their orientation (θ_p) are calculated by:

    [ P = \frac{E}{6d} \left( U_1 + U_2 + U_3 + 2 \sqrt{(U_1 - U_2)^2 + (U_2 - U_3)^2 + (U_3 - U_1)^2} \right) ]

    [ Q = \frac{E}{6d} \left( U_1 + U_2 + U_3 - 2 \sqrt{(U_1 - U_2)^2 + (U_2 - U_3)^2 + (U_3 - U_1)^2} \right) ]

    [ \theta_p = \frac{1}{2} \tan^{-1} \left( \frac{\sqrt{3}(U_2 - U_3)}{2U_1 - U_2 - U_3} \right) ]

  • E = Young’s modulus, d = pilot hole diameter.

  • Overcoring releases stresses, causing measurable deformation, which is related back to in-situ stresses.

This method allows in-situ stress determination around underground openings by analyzing deformation of the borehole wall.

?How are the pilot hole and overcore hole drilled and prepared for testing?

Pilot Hole and Overcore Hole Drilling & Preparation (IS 13946 Part 2)

  • Start drilling with the large overcore bit to the desired depth (Clause 5.2.2).
  • Remove the large core, then use a short pilot hole starter core barrel to drill the pilot hole (Clause 5.2.3).
  • Extend the pilot hole approximately 2 m, ensuring it stays within ±14 mm of the overcore centerline.
  • Avoid fracture zones in the pilot hole area to ensure accurate instrument placement.
  • Proceed with overcoring until the bit passes the cantilever tips by at least 150 mm, preferably 225 mm (Clause 5.2.9).
  • Total overcore length should be about 300-450 mm (2-3 times the overcore hole diameter) to achieve stable gauge readings.
  • Optionally, drill a secondary diamond hole nearby to locate intact rock zones and avoid fractures, saving test time.
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This method ensures accurate stress measurement by maintaining hole alignment and avoiding fractured zones.

?What equipment is required for accurate measurement of rock stress using this method?

Equipment Required for Accurate Rock Stress Measurement (IS 13946 Part 2):

  1. Drill Rods and Drill Bits

    • Pilot hole: 38 mm diameter, drilled with single/double-tube core barrel (~2 m length)
    • Overcoring bit: ~150 mm diameter, mounted on BQ wireline drill rods (55.6 mm o.d.) or equivalent
    • Special stabilizers every ~3 m on drill string to reduce vibrations
    • Overcore diameter: 3-4 times pilot hole diameter to fit modulus chamber
  2. Deformation Gauge (USBM-type)

    • Measures changes in pilot hole diameter in 1 or 3 orientations
    • Detects diameter changes as small as 1 part in 10,000
    • Waterproof, firmly held inside hole, detachable from signal cable
    • Uses cantilever with bonded electric resistance strain gauges
  3. Signal and Readout Equipment

    • Water swivel to allow signal cable passage through drill rods
    • Strain indicator readout bridge and switchgear for data acquisition
  4. Gauge Placement Tools

    • Placement rods marked for depth and orientation to insert gauge accurately
  5. Core Retrieval Tools

    • Core-breaking wedge, core shovel, core puller for extracting rock cores

Summary Table

EquipmentPurposeKey Specs
Drill rods & bitsCreate pilot & overcore holes38 mm pilot, 150 mm overcore dia
USBM Deformation gaugeMeasure hole diameter changesMulti-orientation, waterproof
Water swivelSignal cable passageCompatible with drill rods
Readout bridge & switchgearRecord strain dataHigh sensitivity
Placement rodsAccurate gauge positioningMarked for depth & orientation
Core retrieval toolsExtract rock coresWedge, shovel, puller

Loading diagram...

This setup

?How are Young's modulus and Poisson's ratio determined and used in stress calculations?

Determination and Use of Young's Modulus (E) and Poisson's Ratio (ν) in IS 13946 Part 2

1. Young's Modulus (E):

  • Obtained from biaxial chamber readings (P and U) using the thick-walled cylinder formula:
    [ E = \frac{D^2 - d^2}{2dP} U ]
    where:
    • (D) = diameter of the overcore
    • (d) = diameter of the pilot hole
    • (P) = applied radial pressure
    • (U) = measured change in pilot hole diameter

2. Poisson's Ratio (ν):

  • Measured by conventional laboratory techniques on rock samples.
  • Used in the strain-stress relationship:
    [ \varepsilon_2 = -\frac{\sigma_2 - \nu (P + Q)}{E} ]
    where (\varepsilon_2) is axial strain, (\sigma_2) axial stress, and (P, Q) are principal stresses perpendicular to the hole axis.

3. Usage in Stress Calculations:

  • Young's modulus and Poisson's ratio are essential to relate measured strains (diameter changes) to in situ stresses.
  • Iterative calculations refine (P) and (Q) using measured strains and estimated axial stress.
  • Statistical treatment of multiple measurements yields least squares estimates of stress components.

Summary Diagram: Stress-Strain Relationship in Drillhole

Loading diagram...

Key Takeaway:

  • E links radial deformation to applied pressure.
  • ν accounts for lateral strain effects.
  • Both parameters enable accurate back-calculation of in situ stresses from overcoring deformation data.
?What are the recommended procedures for data recording and reporting of rock stress measurements?

IS 13946 Part 2: Data Recording & Reporting for Rock Stress Measurements

Reporting Requirements (Clauses 7.1 & 7.2)

General Information:

  • Drillhole location, direction, and length.
  • Geotechnical core log with geological/structural details at measurement depths.
  • Description of procedure and equipment (with diagrams/photos).

Detailed Measurement Data:

  • Field data sheets or plots for each overcoring run showing deformation vs. pressure.
  • Estimated principal strains/stresses ( U_1, U_2, U_3 ).
  • Stress-strain curves or radial pressure vs. borehole deformation plots.
  • Tabulation of hole number, orientation, depth, ( U_1, U_2, U_3 ), Young’s modulus ( E ), and Poisson’s ratio ( \nu ).
  • Plots/tabulations of principal stress magnitudes/directions, including statistical parameters (standard error, correlation).
  • Explanation of discrepancies with other data.

Key Calculation Formulas (Clause 6.3)

  • Young’s Modulus from biaxial chamber test:

[ E = \frac{D^2 - d^2}{2dP} \times U ]

where
( D ) = overcore diameter,
( d ) = pilot hole diameter,
( P ) = applied radial pressure,
( U ) = measured change in pilot hole diameter.

  • Stress-strain relation (plane strain isotropic elasticity):

[ U = d (1 - \nu^2) E (P + Q) + 2(P - Q) \cos 2\theta ]


Summary

  • Record all raw data, deformation plots, and elastic properties.
  • Use statistical methods to estimate principal stresses and their uncertainties.
  • Include photographic/diagrammatic evidence of setup and procedures.
  • Report discrepancies with possible explanations.

This ensures comprehensive, reproducible, and verifiable rock stress measurement reporting per IS 13946 Part 2.

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