The document discusses analysis of wedge failures in rock slopes. It defines the geometry of wedges formed by two intersecting planes and the conditions required for wedge failure. The key parameters are:
1) The plunge of the line of intersection must be greater than the average friction angle and less than the dip of the slope face.
2) The line of intersection must dip out of the slope face.
Methods are presented to calculate the factor of safety of wedges considering friction only or incorporating cohesion, friction, and water pressure on the sliding planes. An example calculation is provided to illustrate the application of the equations.
The document provides an analysis of the slope design for an open pit operation submitted by Andrews Surface-Design LTD. West Country Minerals conducted an independent review using software like DIPS, RocLab, RocPlane, and Slide. The analysis examined potential failure mechanisms like planar, wedge, and toppling failures. It also analyzed the stability of individual benches and the overall slope. The review found that some benches would fail without support but adding tension bolts could achieve the target safety factors, particularly if higher bolt tension is used for seismic conditions. Overall, the analysis found the slope design to be stable but recommended some amendments to bolt support and further sensitivity analysis.
1. The document discusses methods for analyzing slope failures in rock masses, including kinematic analysis using stereographic projections.
2. Kinematic analysis involves plotting the orientation of discontinuities like joints, bedding planes, and faults on a stereonet to determine potential failure mechanisms like planar, wedge, and toppling failures.
3. The main types of failures are analyzed based on the dip and dip direction of discontinuities relative to the slope face. Planar failures occur when discontinuities daylight on the slope face, while wedge and toppling failures have specific conditions related to the intersection of two discontinuities or the dip of discontinuities into the slope.
The document discusses failure of engineering materials. It describes that failure is undesirable as it puts lives and economics at risk. While causes of failure are known, prevention is difficult. Common causes are improper material selection, processing, or design flaws. The document then goes on to describe different types of failure like brittle and ductile fracture as well as fatigue failure. It provides details on how these failures occur and how they can be tested and characterized.
1. The document discusses bending deformation that occurs in a straight beam made of a homogeneous material when subjected to bending. It describes how the beam's cross-section and longitudinal lines distort under an applied bending moment.
2. It notes that the bottom of the beam stretches and the top compresses, with a neutral surface in between that does not change length. Key assumptions are presented about how the stress deforms the material.
3. Equations are developed relating normal strain and stress to the beam's geometry and applied bending moment, with stress varying linearly from compression at the top to tension at the bottom. The location of the neutral axis is also described.
This document discusses transverse shear stresses in beams. It begins by explaining how shear stresses develop within beams subjected to transverse loads and defines the internal shear force V. It then discusses how shear stresses cause shear strains that distort the beam's cross-section. The document proceeds to derive the shear formula that relates the shear stress to the internal shear force V and the beam's geometry. It provides examples of applying the shear formula to compute shear stresses in different beam cross-sections.
1. Shear force and bending moment diagrams are analytical tools used to determine the shear force and bending moment values at different points along a beam under loading. These diagrams help with structural design and analysis.
2. The document discusses different types of beams, loads, and support conditions. It provides examples of calculating and drawing shear force and bending moment diagrams for beams with various loading scenarios, including cantilever beams with point loads, simply supported beams with point loads, and overhanging beams with uniform loads.
3. Key steps in drawing the diagrams are outlined, such as using consistent scaling, labeling principal values, and showing sign conventions clearly. The variation in shear force and bending moment is also summarized for different load types
Shear and torsion .. it provide good knowledge in engineering mechanics and strength of material. The students who expert in this I am sure that he can perform well in designing mechanical engineering components.
The document provides an analysis of the slope design for an open pit operation submitted by Andrews Surface-Design LTD. West Country Minerals conducted an independent review using software like DIPS, RocLab, RocPlane, and Slide. The analysis examined potential failure mechanisms like planar, wedge, and toppling failures. It also analyzed the stability of individual benches and the overall slope. The review found that some benches would fail without support but adding tension bolts could achieve the target safety factors, particularly if higher bolt tension is used for seismic conditions. Overall, the analysis found the slope design to be stable but recommended some amendments to bolt support and further sensitivity analysis.
1. The document discusses methods for analyzing slope failures in rock masses, including kinematic analysis using stereographic projections.
2. Kinematic analysis involves plotting the orientation of discontinuities like joints, bedding planes, and faults on a stereonet to determine potential failure mechanisms like planar, wedge, and toppling failures.
3. The main types of failures are analyzed based on the dip and dip direction of discontinuities relative to the slope face. Planar failures occur when discontinuities daylight on the slope face, while wedge and toppling failures have specific conditions related to the intersection of two discontinuities or the dip of discontinuities into the slope.
The document discusses failure of engineering materials. It describes that failure is undesirable as it puts lives and economics at risk. While causes of failure are known, prevention is difficult. Common causes are improper material selection, processing, or design flaws. The document then goes on to describe different types of failure like brittle and ductile fracture as well as fatigue failure. It provides details on how these failures occur and how they can be tested and characterized.
1. The document discusses bending deformation that occurs in a straight beam made of a homogeneous material when subjected to bending. It describes how the beam's cross-section and longitudinal lines distort under an applied bending moment.
2. It notes that the bottom of the beam stretches and the top compresses, with a neutral surface in between that does not change length. Key assumptions are presented about how the stress deforms the material.
3. Equations are developed relating normal strain and stress to the beam's geometry and applied bending moment, with stress varying linearly from compression at the top to tension at the bottom. The location of the neutral axis is also described.
This document discusses transverse shear stresses in beams. It begins by explaining how shear stresses develop within beams subjected to transverse loads and defines the internal shear force V. It then discusses how shear stresses cause shear strains that distort the beam's cross-section. The document proceeds to derive the shear formula that relates the shear stress to the internal shear force V and the beam's geometry. It provides examples of applying the shear formula to compute shear stresses in different beam cross-sections.
1. Shear force and bending moment diagrams are analytical tools used to determine the shear force and bending moment values at different points along a beam under loading. These diagrams help with structural design and analysis.
2. The document discusses different types of beams, loads, and support conditions. It provides examples of calculating and drawing shear force and bending moment diagrams for beams with various loading scenarios, including cantilever beams with point loads, simply supported beams with point loads, and overhanging beams with uniform loads.
3. Key steps in drawing the diagrams are outlined, such as using consistent scaling, labeling principal values, and showing sign conventions clearly. The variation in shear force and bending moment is also summarized for different load types
Shear and torsion .. it provide good knowledge in engineering mechanics and strength of material. The students who expert in this I am sure that he can perform well in designing mechanical engineering components.
RocPlane is a software tool for analyzing the stability of planar failures in rock slopes. It models a wedge-shaped failure bounded by a sliding plane, slope face, optional tension crack, and upper ground surface. The software can evaluate stability deterministically or probabilistically, accounting for shear strengths, water pressures, external forces, and support measures. It allows flexible definition of wedge geometry and variations in parameters to understand their effects on stability.
The document provides information about mechanics of solids-I, including:
1) It describes different types of supports like simple supports, roller supports, pin-joint supports, and fixed supports. It also describes different types of loads like concentrated loads, uniformly distributed loads, and uniformly varying loads.
2) It discusses shear force as the unbalanced vertical force on one side of a beam section, and bending moment as the sum of moments about a section.
3) It explains the relationship between loading (w), shear force (F), and bending moment (M) for an element of a beam. The rate of change of shear force is equal to the loading intensity, and the rate of change of bending
VORTEX DYNAMIC INVESTIGATION OF WING SLOTTED GAP OF SAAB JAS GRIPEN C-LIKE FI...IAEME Publication
Canard fighters generally configured with wing canard-deltas and would generate
an airflow phenomenon producing vortex cores and lifts. The lift distribution would
stall at a high angle of attack (AoA). This study investigated the vortex dynamic of
wing canard delta configurations of the Saab JAS Gripen C-like model which create
different wing planform than other fighters. The slotted leading edge of the Gripen
would develop a strong vortex core on the outer wing, on the same direction with the
spin of wing vortex; the outer core would drag the inner vortex core and strengthened.
Consequently, the vortex core streamlined in a leading edge of the wing would begin
to detach, resulting rolled-up vortices in the wing leading edge followed by a solid
laminar stream which tends to curl out. The trailing edge of the wing tended to
laminarize backward. The result would be a negative surface pressure on the leading
edge above the canard and on the wing which causes more negative surface pressures.
An increase in AoA will generate a closer vortex breakdown location to the wing
leading edge. The location was calculated as the ratio of the axial velocity
Comparative Study on Anchorage in Reinforced Concrete Using Codes of Practice...IJERA Editor
This paper (Part II) reports a comparative study for BS8110 and EC2 of practice and those expressions by Batayneh and Neilsen on tests from literature. These have been treated under straight bar anchorages with transverse pressure. The aim of this study is to evaluate the reliability of the existing equations for bond strength of straight bars by applying to the available tests in the literature .The most important parameters were examined in these tests are concrete strength, anchorage length, concrete covers, bar diameter and transverse pressure. 264 tests from the literature have been chosen, which are all for straight bars with transverse pressure. The specimens are pull-out specimens with small concrete covers, beams ends and slabs. For both comparative studies in Part I and Part II, the conclusions and recommendations are presented here together.
The document discusses design considerations for machine elements subjected to fluctuating loads. It covers topics such as stress concentration, fatigue failure, endurance limit, factors affecting fatigue strength, and methods to reduce stress concentration and improve fatigue life. Stress concentration occurs due to discontinuities and can be reduced by avoiding abrupt changes in cross-section and providing fillets. Fatigue failure is caused by fluctuating stresses and depends on factors like the number of cycles and mean stress. The endurance limit is the maximum stress amplitude a material can withstand without failure under completely reversed loading. Surface finish, size, and mean stress affect the endurance limit.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as the localization of high stresses due to irregularities or abrupt changes in cross-section. Stress concentration can be reduced by avoiding sharp changes in cross-section and providing fillets and chamfers. Fatigue failure occurs when fluctuating stresses cause cracks over numerous load cycles. The endurance limit is the maximum stress amplitude that causes failure after an infinite number of cycles. Factors like stress concentration, surface finish, size, and mean stress affect the endurance limit. Designs should minimize stress raisers and protect against corrosion to prevent fatigue failures.
Design methods for torsional buckling of steel structuresBegum Emte Ajom
The document discusses methods for designing steel structures to resist torsional buckling. It summarizes clauses from Eurocode 3 that provide equations for calculating the elastic critical buckling moment and determining the reduction factor used to calculate the design bending strength. It also presents simplified equations that can be used to calculate the elastic critical buckling moment for common steel beam sections. Additional guidance is provided for calculating the critical buckling moment for non-symmetric sections and when bending occurs about the major axis.
Analysis of Multi-storey Building Frames Subjected to Gravity and Seismic Loa...Pralhad Kore
This document summarizes the results of analyzing 3-bay, 5-bay, and 7-bay 9-story reinforced concrete frames with varying geometric properties under gravity and seismic loads. The response of frames was studied when incorporating idealized T-beams between points of contraflexure in beams and providing haunches of varying widths at beam-column joints. Results found that axial forces in columns increased linearly from top to bottom, while bending moments decreased with larger beam-column stiffness ratios. Lateral displacements under seismic loads were reduced by incorporating T-beams and haunches, demonstrating their beneficial effects on structural response.
Analysis of multi storey building frames subjected to gravity and seismic loa...Pralhad Kore
This document summarizes a study on the seismic response of reinforced concrete frames with varying numbers of bays and storeys. Three frame configurations - 3 bay, 5 bay, and 7 bay with 9 stories each - were modeled and analyzed under gravity and seismic loads. Both prismatic frames and frames with non-prismatic elements like stepped beams and haunches at beam-column joints were considered. The effects of variables like haunch size, beam inertia, and live load patterns on internal forces and storey drift were examined. Key results showed that non-prismatic elements can reduce bending moments and axial forces compared to conventional prismatic frames.
Prediction of Small Size Pneumatic Tyres for Tyre Traction PropertiesIDES Editor
An analytical approach for determining tyre force
and moment characteristics due to pure slips has been
presented. The analytical model predicts these forces and
moments in terms of easily measurable tyre parameters such
as contact patch area, lateral, longitudinal, and vertical
stiffnesses of tyre. These analytical predictions show good
agreement with existing measured data. The model is suitable
for study of vehicle dynamic simulations.
Approximate Analysis of Statically Indeteminate Structures.pdfAshrafZaman33
This document discusses approximate analysis methods for statically indeterminate structures like trusses and frames. It introduces the concept of making a structure statically determinate by assuming certain members carry zero force, then analyzing the simplified structure. Two common assumptions are mentioned: (1) slender diagonals cannot carry compression, and (2) diagonals share the panel load equally between tension and compression. Examples show how to apply these methods to trusses. The document also discusses analyzing building frames by assuming points of inflection act as pins, then using superposition to account for multiple load cases.
This document discusses the design of tension members according to IS 800-2007. It defines tension members as structural elements subjected to direct axial tensile loads. Tension members can fail due to gross section yielding, net section rupture, or block shear failure. The document describes various types of tension members including wires, bars, plates, structural shapes, and their behavior under tensile loads. It provides equations to calculate the design strength based on the different failure modes and discusses factors like slenderness ratio and shear lag that influence tension member design. Numerical examples are given to illustrate the design strength calculations.
Compression members are structural members subjected to axial compression or compressive forces. Their design is governed by strength and buckling capacity. Columns can fail due to local buckling, squashing, overall flexural buckling, or torsional buckling. Built-up columns use components like lacings, battens, and cover plates to help distribute stress more evenly and increase buckling resistance compared to a single member. Buckling occurs when a straight compression member becomes unstable and bends under a critical load.
This research aims to analyze how ground accelerations within liquefiable soils affect inelastic structures through physical and numerical modeling of a 3-story moment-resisting frame. Prior component testing of a beam-column connection will help validate numerical models and ensure the physical model captures real building behavior. A connection design with a structural fuse is being tested under cyclic loading to understand moment-rotation response. Future tests will integrate the frame into liquefiable soil models in a centrifuge to study soil-structure interaction and mitigation techniques during earthquakes.
A study-of-the-behaviour-of-overlying-strata-in-longwall-mining-and-its-appli...Agustino Rosas
This study investigated the behavior of rock strata above a longwall coal mining face. Instruments were installed in boreholes above an active longwall face in China to monitor the movement of rock layers over time. The data showed three zones of behavior: 1) an abutment pressure zone with little movement near the face, 2) a bed separation zone where rock layers began to separate as the face passed, and 3) a consolidation zone further away where the layers reconsolidated. By analyzing the displacement curves, a structural model was created to examine how forces are distributed between the rock blocks as mining progresses. This model can help explain some phenomena observed during longwall mining such as ground subsidence and roof pressure development.
A study-of-the-behaviour-of-overlying-strata-in-longwall-mining-and-its-appli...Agustino Rosas
This study investigated the behavior of rock strata above a longwall coal mining face. Instruments were installed in boreholes above an active longwall panel in China to monitor the movement of plugs placed between different rock layers. The investigation found that as the longwall face approached and passed beneath a monitoring point, the overlying strata could be divided into three zones: (1) an abutment pressure zone with minor movement, (2) a bed separation zone where rock layers began to separate from each other with increasing movement rates, and (3) a consolidation zone further behind the face where the separated layers reconsolidated with decreasing movement rates. Analyzing the displacement curves of the plugs allowed constructing a structural model to explain
1) The document discusses torsion and torsional deformation of circular shafts. It derives the torsion formula which relates the shear stress in a shaft to the torque and geometry of the shaft's cross section.
2) Power transmission using shafts is discussed. The relationship between torque, angular velocity, and power is defined. Shaft design using the torsion formula and allowable shear stress is also covered.
3) Examples are presented to demonstrate calculating shear stresses and designing shafts given torque and power transmission information.
This document provides an overview of the design of compression members (columns) in reinforced concrete structures. It discusses various types of columns based on reinforcement, loading conditions, and slenderness ratio. It describes the classification of columns as short or slender. The document also covers effective length, braced vs unbraced columns, codal provisions for reinforcement, and functions of longitudinal and transverse reinforcement. Key points include types of column reinforcement, minimum reinforcement requirements, cover requirements, and assumptions for the limit state of collapse under compression.
6.KESTABILAN pada LONGSOR BIDANG 2022.pdfBelajar50
This document discusses methods for analyzing plane slope failures through limit equilibrium analysis. It provides equations and explanations for:
1. The general conditions required for a plane failure, including the geometry of the sliding plane and release surfaces.
2. Calculating the factor of safety for plane failures using equations that consider the forces acting on the potential sliding mass, including weight, water pressures, and shear strength. Critical locations and inclinations of tension cracks that could lead to failure are also analyzed.
3. The influence of groundwater conditions on stability, including possible pressure distributions within tension cracks and along sliding planes.
The analyses make assumptions about force distributions and water pressures to provide methods for quantifying slope stability under different conditions
RocPlane is a software tool for analyzing the stability of planar failures in rock slopes. It models a wedge-shaped failure bounded by a sliding plane, slope face, optional tension crack, and upper ground surface. The software can evaluate stability deterministically or probabilistically, accounting for shear strengths, water pressures, external forces, and support measures. It allows flexible definition of wedge geometry and variations in parameters to understand their effects on stability.
The document provides information about mechanics of solids-I, including:
1) It describes different types of supports like simple supports, roller supports, pin-joint supports, and fixed supports. It also describes different types of loads like concentrated loads, uniformly distributed loads, and uniformly varying loads.
2) It discusses shear force as the unbalanced vertical force on one side of a beam section, and bending moment as the sum of moments about a section.
3) It explains the relationship between loading (w), shear force (F), and bending moment (M) for an element of a beam. The rate of change of shear force is equal to the loading intensity, and the rate of change of bending
VORTEX DYNAMIC INVESTIGATION OF WING SLOTTED GAP OF SAAB JAS GRIPEN C-LIKE FI...IAEME Publication
Canard fighters generally configured with wing canard-deltas and would generate
an airflow phenomenon producing vortex cores and lifts. The lift distribution would
stall at a high angle of attack (AoA). This study investigated the vortex dynamic of
wing canard delta configurations of the Saab JAS Gripen C-like model which create
different wing planform than other fighters. The slotted leading edge of the Gripen
would develop a strong vortex core on the outer wing, on the same direction with the
spin of wing vortex; the outer core would drag the inner vortex core and strengthened.
Consequently, the vortex core streamlined in a leading edge of the wing would begin
to detach, resulting rolled-up vortices in the wing leading edge followed by a solid
laminar stream which tends to curl out. The trailing edge of the wing tended to
laminarize backward. The result would be a negative surface pressure on the leading
edge above the canard and on the wing which causes more negative surface pressures.
An increase in AoA will generate a closer vortex breakdown location to the wing
leading edge. The location was calculated as the ratio of the axial velocity
Comparative Study on Anchorage in Reinforced Concrete Using Codes of Practice...IJERA Editor
This paper (Part II) reports a comparative study for BS8110 and EC2 of practice and those expressions by Batayneh and Neilsen on tests from literature. These have been treated under straight bar anchorages with transverse pressure. The aim of this study is to evaluate the reliability of the existing equations for bond strength of straight bars by applying to the available tests in the literature .The most important parameters were examined in these tests are concrete strength, anchorage length, concrete covers, bar diameter and transverse pressure. 264 tests from the literature have been chosen, which are all for straight bars with transverse pressure. The specimens are pull-out specimens with small concrete covers, beams ends and slabs. For both comparative studies in Part I and Part II, the conclusions and recommendations are presented here together.
The document discusses design considerations for machine elements subjected to fluctuating loads. It covers topics such as stress concentration, fatigue failure, endurance limit, factors affecting fatigue strength, and methods to reduce stress concentration and improve fatigue life. Stress concentration occurs due to discontinuities and can be reduced by avoiding abrupt changes in cross-section and providing fillets. Fatigue failure is caused by fluctuating stresses and depends on factors like the number of cycles and mean stress. The endurance limit is the maximum stress amplitude a material can withstand without failure under completely reversed loading. Surface finish, size, and mean stress affect the endurance limit.
The document discusses stress concentration and fatigue failure in machine elements. It defines stress concentration as the localization of high stresses due to irregularities or abrupt changes in cross-section. Stress concentration can be reduced by avoiding sharp changes in cross-section and providing fillets and chamfers. Fatigue failure occurs when fluctuating stresses cause cracks over numerous load cycles. The endurance limit is the maximum stress amplitude that causes failure after an infinite number of cycles. Factors like stress concentration, surface finish, size, and mean stress affect the endurance limit. Designs should minimize stress raisers and protect against corrosion to prevent fatigue failures.
Design methods for torsional buckling of steel structuresBegum Emte Ajom
The document discusses methods for designing steel structures to resist torsional buckling. It summarizes clauses from Eurocode 3 that provide equations for calculating the elastic critical buckling moment and determining the reduction factor used to calculate the design bending strength. It also presents simplified equations that can be used to calculate the elastic critical buckling moment for common steel beam sections. Additional guidance is provided for calculating the critical buckling moment for non-symmetric sections and when bending occurs about the major axis.
Analysis of Multi-storey Building Frames Subjected to Gravity and Seismic Loa...Pralhad Kore
This document summarizes the results of analyzing 3-bay, 5-bay, and 7-bay 9-story reinforced concrete frames with varying geometric properties under gravity and seismic loads. The response of frames was studied when incorporating idealized T-beams between points of contraflexure in beams and providing haunches of varying widths at beam-column joints. Results found that axial forces in columns increased linearly from top to bottom, while bending moments decreased with larger beam-column stiffness ratios. Lateral displacements under seismic loads were reduced by incorporating T-beams and haunches, demonstrating their beneficial effects on structural response.
Analysis of multi storey building frames subjected to gravity and seismic loa...Pralhad Kore
This document summarizes a study on the seismic response of reinforced concrete frames with varying numbers of bays and storeys. Three frame configurations - 3 bay, 5 bay, and 7 bay with 9 stories each - were modeled and analyzed under gravity and seismic loads. Both prismatic frames and frames with non-prismatic elements like stepped beams and haunches at beam-column joints were considered. The effects of variables like haunch size, beam inertia, and live load patterns on internal forces and storey drift were examined. Key results showed that non-prismatic elements can reduce bending moments and axial forces compared to conventional prismatic frames.
Prediction of Small Size Pneumatic Tyres for Tyre Traction PropertiesIDES Editor
An analytical approach for determining tyre force
and moment characteristics due to pure slips has been
presented. The analytical model predicts these forces and
moments in terms of easily measurable tyre parameters such
as contact patch area, lateral, longitudinal, and vertical
stiffnesses of tyre. These analytical predictions show good
agreement with existing measured data. The model is suitable
for study of vehicle dynamic simulations.
Approximate Analysis of Statically Indeteminate Structures.pdfAshrafZaman33
This document discusses approximate analysis methods for statically indeterminate structures like trusses and frames. It introduces the concept of making a structure statically determinate by assuming certain members carry zero force, then analyzing the simplified structure. Two common assumptions are mentioned: (1) slender diagonals cannot carry compression, and (2) diagonals share the panel load equally between tension and compression. Examples show how to apply these methods to trusses. The document also discusses analyzing building frames by assuming points of inflection act as pins, then using superposition to account for multiple load cases.
This document discusses the design of tension members according to IS 800-2007. It defines tension members as structural elements subjected to direct axial tensile loads. Tension members can fail due to gross section yielding, net section rupture, or block shear failure. The document describes various types of tension members including wires, bars, plates, structural shapes, and their behavior under tensile loads. It provides equations to calculate the design strength based on the different failure modes and discusses factors like slenderness ratio and shear lag that influence tension member design. Numerical examples are given to illustrate the design strength calculations.
Compression members are structural members subjected to axial compression or compressive forces. Their design is governed by strength and buckling capacity. Columns can fail due to local buckling, squashing, overall flexural buckling, or torsional buckling. Built-up columns use components like lacings, battens, and cover plates to help distribute stress more evenly and increase buckling resistance compared to a single member. Buckling occurs when a straight compression member becomes unstable and bends under a critical load.
This research aims to analyze how ground accelerations within liquefiable soils affect inelastic structures through physical and numerical modeling of a 3-story moment-resisting frame. Prior component testing of a beam-column connection will help validate numerical models and ensure the physical model captures real building behavior. A connection design with a structural fuse is being tested under cyclic loading to understand moment-rotation response. Future tests will integrate the frame into liquefiable soil models in a centrifuge to study soil-structure interaction and mitigation techniques during earthquakes.
A study-of-the-behaviour-of-overlying-strata-in-longwall-mining-and-its-appli...Agustino Rosas
This study investigated the behavior of rock strata above a longwall coal mining face. Instruments were installed in boreholes above an active longwall face in China to monitor the movement of rock layers over time. The data showed three zones of behavior: 1) an abutment pressure zone with little movement near the face, 2) a bed separation zone where rock layers began to separate as the face passed, and 3) a consolidation zone further away where the layers reconsolidated. By analyzing the displacement curves, a structural model was created to examine how forces are distributed between the rock blocks as mining progresses. This model can help explain some phenomena observed during longwall mining such as ground subsidence and roof pressure development.
A study-of-the-behaviour-of-overlying-strata-in-longwall-mining-and-its-appli...Agustino Rosas
This study investigated the behavior of rock strata above a longwall coal mining face. Instruments were installed in boreholes above an active longwall panel in China to monitor the movement of plugs placed between different rock layers. The investigation found that as the longwall face approached and passed beneath a monitoring point, the overlying strata could be divided into three zones: (1) an abutment pressure zone with minor movement, (2) a bed separation zone where rock layers began to separate from each other with increasing movement rates, and (3) a consolidation zone further behind the face where the separated layers reconsolidated with decreasing movement rates. Analyzing the displacement curves of the plugs allowed constructing a structural model to explain
1) The document discusses torsion and torsional deformation of circular shafts. It derives the torsion formula which relates the shear stress in a shaft to the torque and geometry of the shaft's cross section.
2) Power transmission using shafts is discussed. The relationship between torque, angular velocity, and power is defined. Shaft design using the torsion formula and allowable shear stress is also covered.
3) Examples are presented to demonstrate calculating shear stresses and designing shafts given torque and power transmission information.
This document provides an overview of the design of compression members (columns) in reinforced concrete structures. It discusses various types of columns based on reinforcement, loading conditions, and slenderness ratio. It describes the classification of columns as short or slender. The document also covers effective length, braced vs unbraced columns, codal provisions for reinforcement, and functions of longitudinal and transverse reinforcement. Key points include types of column reinforcement, minimum reinforcement requirements, cover requirements, and assumptions for the limit state of collapse under compression.
Similar to 7.KESTABILAN pada LONGSOR BAJI.pdf (20)
6.KESTABILAN pada LONGSOR BIDANG 2022.pdfBelajar50
This document discusses methods for analyzing plane slope failures through limit equilibrium analysis. It provides equations and explanations for:
1. The general conditions required for a plane failure, including the geometry of the sliding plane and release surfaces.
2. Calculating the factor of safety for plane failures using equations that consider the forces acting on the potential sliding mass, including weight, water pressures, and shear strength. Critical locations and inclinations of tension cracks that could lead to failure are also analyzed.
3. The influence of groundwater conditions on stability, including possible pressure distributions within tension cracks and along sliding planes.
The analyses make assumptions about force distributions and water pressures to provide methods for quantifying slope stability under different conditions
Batuan dan tanah memiliki karakteristik yang berbeda berdasarkan kekuatan dan komposisinya. Batuan terbentuk dari proses magmatik, sedimentasi, dan metamorfosis, sedangkan tanah terbentuk dari pelapukan batuan. Cacat pada batuan seperti perlapisan, sesar, dan lipatan dapat mempengaruhi kekuatan dan kestabilan batuan.
ISO/IEC 27001, ISO/IEC 42001, and GDPR: Best Practices for Implementation and...PECB
Denis is a dynamic and results-driven Chief Information Officer (CIO) with a distinguished career spanning information systems analysis and technical project management. With a proven track record of spearheading the design and delivery of cutting-edge Information Management solutions, he has consistently elevated business operations, streamlined reporting functions, and maximized process efficiency.
Certified as an ISO/IEC 27001: Information Security Management Systems (ISMS) Lead Implementer, Data Protection Officer, and Cyber Risks Analyst, Denis brings a heightened focus on data security, privacy, and cyber resilience to every endeavor.
His expertise extends across a diverse spectrum of reporting, database, and web development applications, underpinned by an exceptional grasp of data storage and virtualization technologies. His proficiency in application testing, database administration, and data cleansing ensures seamless execution of complex projects.
What sets Denis apart is his comprehensive understanding of Business and Systems Analysis technologies, honed through involvement in all phases of the Software Development Lifecycle (SDLC). From meticulous requirements gathering to precise analysis, innovative design, rigorous development, thorough testing, and successful implementation, he has consistently delivered exceptional results.
Throughout his career, he has taken on multifaceted roles, from leading technical project management teams to owning solutions that drive operational excellence. His conscientious and proactive approach is unwavering, whether he is working independently or collaboratively within a team. His ability to connect with colleagues on a personal level underscores his commitment to fostering a harmonious and productive workplace environment.
Date: May 29, 2024
Tags: Information Security, ISO/IEC 27001, ISO/IEC 42001, Artificial Intelligence, GDPR
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How to Setup Warehouse & Location in Odoo 17 InventoryCeline George
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2. Wedge failure
8.1 INTRODUCTION
Chapter 7 dealt with slope failure resulting from sliding on a single planar surface dipping out of the face,
and striking parallel or nearly parallel to the slope face. It was stated that the plane failure analysis is valid if
the strike of the failure plane is within ±20° of the strike of the slope face. This chapter is concerned with the
failure of slopes containing discontinuities striking obliquely to the slope face where sliding of a wedge of
rock takes place along the line of intersection of two such planes (Figure 8.1). Wedge failures can occur
over a much wider range of geologic and geometric conditions than plane failures. Therefore, the study of
wedge stability is an important component of rock slope engineering. The analysis of wedges has been
extensively discussed in geotechnical literature, and this chapter draws heavily upon the work of Goodman
(1964), Wittke (1965), Londe (1965), Londe, Vigier and Vormeringer (1969, 1970) and John (1970).
In this chapter, the structural geological conditions that result in the formation of a wedge formed by two
intersecting planes are defined, and the method of identifying wedges on the stereonet is illustrated. The
stereonet defines the shape of the wedge, the orientation of the line of intersection and the direction of
sliding, but not the dimensions. This information can be used to assess the potential for the wedge to slide
from the cut face. The procedure is termed kinematic analysis, the purpose of which is to identify
potentially unstable wedges, although it does not provide precise information on their factor of safety.
3. The chapter presents design charts that can be used to find the factor of safety of wedges for which
friction is the only component of the shear strength, and no external forces such as water pressures or
bolting act on the wedge. In addition, equations are presented that can be used to calculate the factor of
safety of wedges where the shear strength on the two slide planes is defined by cohesion and friction
angle, and each plane can have different shear strengths. The analysis can also incorporate water
pressure.
The presence of a tension crack, and the influence of external forces due to water pressures, tensioned
anchors, seismic accelerations or bridge foundations results in a significant increase in the complexity of
the equations. Appendix III presents the complete solution for the wedge analysis.
4. 8.2 DEFINITION OF WEDGE GEOMETRY
Typical wedge failures, illustrated in Figures 8.1 and 8.2,
show the conditions that are normally assumed for the
analytical treatment of wedges. Figure 8.1 shows a cut slope
in granitic rock where a wedge is formed by two continuous,
planar discontinuities and the line of intersection of these
two planes daylights just at the toe of the rock face. That is,
the trend of the line of intersection and the dip direction of
the face are approximately equal. Furthermore, the plunge
of the line of intersection is about 50–55°, while the friction
angle of these joints is in the range of 35–40°. That is, the
line of intersection dips steeper than the friction angle.
These conditions meet the kinematic requirements for failure
of the wedge. Figure 8.1 also illustrates how a slight change
in the site conditions would result in a stable slope. For
example, if the line of intersection had been slightly behind
the face, or just one of the joints had been discontinuous,
then no failure would have occurred.
Figure 8.1 Typical wedge failure involving sliding on two persistent joints with
line of intersection of joints daylighting at toe of rock face, and an upper plane
that formed a tension crack (strong, volcanic rock on Interstate 5, near Grants
Pass, Oregon).
5. The wedge in Figure 8.2 is formed by
bedding on the left and a conjugate
joint set on the right. As seen in
Figure 8.1, the line of intersection
daylights in the slope face and failure
occurred. However, in this wedge,
sliding occurred almost entirely on
the bedding with the joint acting as a
release surface. Therefore, the shear
strength of the joint has little effect on
stability.
Figure 8.1 Typical wedge failure involving sliding on two persistent joints with line
of intersection of joints daylighting at toe of rock face, and an upper plane that
formed a tension crack (strong, volcanic rock on Interstate 5, near Grants Pass,
Oregon).
6. The geometry of the wedge for analysing the basic
mechanics of sliding is defined in Figure 8.3. Based on
this geometry, the general conditions for wedge failure
are as follows:
1. Two planes will always intersect in a line (Figure
8.3a). On the stereonet, the line of intersection is
represented by the point where the two great circles of
the planes intersect, and the orientation of the line is
defined by its trend (ai) and its plunge (yi) (Figure 8.3b).
Figure 8.3 Geometric conditions for wedge failure:
(a) pictorial view of wedge failure; (b) stereoplot
showing the orientation of the line of intersection,
and the range of the plunge of the line of
intersection ψi where failure is feasible;
7. 2. The plunge of the line of intersection must be flatter than the dip of
the face, and steeper than the average friction angle of the two slide
planes, that is, yf > yi > ϕ (Figure 8.3b and c). The inclination of the
slope face yf is measured in the view at right angles to the line of
intersection. Note that the yf i would only be the same as yf, the true
dip of the slope face, if the trend of the line of intersection was the
same as the dip direction of the slope face.
3. The line of intersection must dip in a direction out of the face for
sliding to be feasible; the possible range in the trend of the line of
intersection is between ai and ai’ (Figure 8.3d).
Figure 8.3 Geometric conditions for wedge
failure: (c) view of slope at right angles to the
line of intersection; (d) stereonet showing the
range in the trend of the line of intersection αi
where wedge failure is feasible.
8. Figure 8.3 Geometric conditions for wedge failure: (a)
pictorial view of wedge failure; (b) stereoplot showing
the orientation of the line of intersection, and the range
of the plunge of the line of intersection yi where failure
is feasible; (c) view of slope at right angles to the line of
intersection; (d) stereonet showing the range in the
trend of the line of intersection αi where wedge failure
is feasible.
9. In general, sliding may occur if the intersection point
between the two great circles of the sliding planes lies
within the shaded area in Figure 8.3b. That is, the
stereonet will show whether wedge failure is
kinematically feasible. However, the actual factor of
safety of the wedge cannot be determined from the
stereonet, because it depends on the details of the
geometry of the wedge, the shear strength of each
plane and water pressure, as described in the following
sections.
The trend ai and plunge yi of the line of intersection of
planes A and B can be determined on the stereonet, or
calculated using Equations 8.1 and 8.2 as follows:
(8.1)
(8.2)
where aA and aB are the dip directions
and yA and yB are the dips of the two
planes. Equation 8.1 gives two
solutions 180° apart; the correct value
lies between aA and aB.
10. 8.3 ANALYSIS OF WEDGE FAILURE
The factor of safety of the wedge defined in Figure 8.3,
assuming that sliding is resisted only by friction and that the
friction angle ϕ is the same for both planes, is given by
(8.3)
where RA and RB are the normal reactions provided by planes A and B as illustrated in Figure
8.4, and the component of the weight acting down the line of intersection is (W·sin yi). The
forces RA and RB are found by resolving them into components normal and parallel to the
direction along the line of intersection as follows:
where the angles ξ and β are defined in Figure 8.4a. Angles ξ and β are measured on the
great circle containing the pole to the line of intersection and the poles of the two slide
planes. In order to meet the conditions for equilibrium, the normal components of the
reactions are equal (Equation 8.4), and the sum of the parallel components equals the
component of the weight acting down the line of intersection (Equation 8.5).
(8.4)
(8.5)
11. Figure 8.4 Resolution of forces to calculate factor of safety of wedge: (a) view of wedge looking at face showing definition of angle β and
ξ, and reactions on sliding planes RA and RB; (b) stereonet showing measurement of angles β and ξ; (c) cross-section of wedge showing
resolution of wedge weight W on the line of intersection.
The values of RA and RB are found from Equations 8.4 and 8.5 by solving and adding as follows:
Hence, In other words,
where FSW is the factor of safety of a wedge supported by friction only, and FSp is the factor of safety of a plane
failure in which the slide plane, with friction angle ϕ, dips at the same angle as the line of intersection yi.
(8.6) (8.7) (8.8)
12. K is the wedge factor that, as shown by
Equation 8.7, depends upon the included
angle of the wedge ξ and the angle of tilt
β of the wedge. Values for the wedge
factor K, for a range of values of ξ and β,
are plotted in Figure 8.5.
Figure 8.5 Wedge factor K as a function of wedge geometry.
13. The method of calculating the factor of safety of wedges as discussed in this section is, of course,
simplistic because it does not incorporate different friction angles and cohesions on the two slide planes,
or ground water pressures. When these factors are included in the analysis, the equations become more
complex. Rather than developing these equations in terms of the angles ξ and β, which cannot be
measured directly in the field, the more complete analysis is presented in terms of directly measurable
dips and dip directions. The following section gives equations for the factor of safety of a wedge with
cohesion and friction acting on the slide planes and water pressure. The complete set of equations for
stability analysis of a wedge is shown in Appendix III; this analysis includes parameters to define the
shape and dimensions of the wedge, different shear strengths on each slide surface, water pressures
and two external loads.
This section shows the important influence of the wedging action as the included angle of the wedge
decreases below 90°. The increase by a factor of 2 or 3 on the factor safety determined by plane failure
analysis is of great practical importance because, as shown in Figure 8.5, the factor of safety of a wedge
can be significantly greater than that of a plane failure (i.e., K > 1). Therefore, where the structural
features that are likely to control the stability of a rock slope do not strike parallel to the slope face, the
stability analysis should be carried out by means of 3D methods discussed in this chapter.
14. 8.4 WEDGE ANALYSIS INCLUDING COHESION, FRICTION AND WATER PRESSURE
Section 8.3 discussed the geometric conditions that could result in a wedge failure, but this kinematic analysis provides
limited information of the factor of safety because the dimensions of the wedge were not considered. This section
describes a method to calculate the factor of safety of a wedge that incorporates the slope geometry, different
shear strengths of the two slide planes and ground water (Hoek, Bray and Boyd, 1973). However, the limitations of
this analysis are that it does not include a tension crack, or external forces such as bolting.
Figure 8.6a shows the geometry and dimensions of the wedge
that will be considered in the following analysis, with the five
numbered lines that define the shape of the wedge. Note that the
upper slope surface in this analysis can be obliquely inclined with
respect to the slope face, thereby removing a restriction that has
been present in the stability analyses that have been discussed
so far in the book. The total height of the slope H is the difference
in vertical elevation between the upper and lower extremities of
the line of intersection along which sliding is assumed to occur.
The water pressure distribution assumed for this analysis is based
upon the hypothesis that the wedge itself is impermeable and that
water enters the top of the wedge along lines of intersections 3
and 4 and discharges to the atmosphere from the slope face
along lines of intersections 1 and 2.
Figure 8.6 Geometry of wedge used for stability analysis
including the influence of friction and cohesion, and of water
pressure on the slide surfaces: (a) pictorial view of wedge
showing the numbering of the intersection lines and plane;
15. The resulting pressure distribution is shown in Figure 8.6b – the
maximum pressure occurring along the line of intersection 5 and
the pressure being zero along lines 1, 2, 3 and 4. This is a
triangular pressure distribution with the maximum value occurring
at the mid-height of the slope, with the estimated maximum
pressure being equal to (1/2 · gw · H). This water pressure
distribution is believed to be representative of the extreme
conditions that could occur during heavy rain and the slope is
saturated.
Figure 8.6 Geometry of wedge used for stability analysis
including the influence of friction and cohesion, and of
water pressure on the slide surfaces: (b) view normal to the
line of intersection (5) showing wedge height and water
pressure distribution.
The two planes on which sliding occurs are designated A and B,
with plane A having the shallower dip. The numbering of the five
lines of intersection of the four planes defining the wedge is as
follows:
Line 1. Intersection of plane A with the slope face
Line 2. Intersection of plane B with the slope face
Line 3. Intersection of plane A with upper slope surface
Line 4. Intersection of plane B with upper slope surface
Line 5. Intersection of planes A and B
16. It is assumed that sliding of the wedge always takes place along the line of intersection numbered 5, and
its factor of safety is given by (Hoek, Bray and Boyd, 1973)
(8.9)
where cA and cB are the cohesive strengths, and ϕA and ϕB are the angles of friction, respectively, on
planes A and B; gr is the unit weight of the rock, gw the unit weight of the water and H the total height of
the wedge measured along the line of intersection 5. The dimensionless factors X, Y, A and B depend
upon the geometry of the wedge.
The values of parameters X, Y, A and B are given in Equations 8.10 to 8.13
(8.13)
(8.12)
(8.11)
(8.10)
where ya and yb are the dips of planes A and B,
respectively, and y5 is the dip of the line of
intersection, line 5. The angles required for the
solution of these equations can be measured most
conveniently on a stereoplot that defines the geometry
of the wedge and the slope (Figure 8.7).
17. Figure 8.7 Stereoplot of data required for wedge stability analysis.
The application of the equations discussed in this
section is illustrated in the following example,
using the parameters shown in Table 8.1.
The total height of the wedge H is 40 m (131 ft), the
unit weight of the rock is 25 kN/m3 (165 lb/ft3) and
the unit weight of the water 9.81 kN/m3 (62.5 lb/ft3).
The stereoplot of the great circles representing
the four planes involved in this example is
presented in Figure 8.7, and all the angles
required for the solution of Equations 8.10 to 8.13
are marked in this figure.
Determination of the factor of safety is most
conveniently carried out on a spread sheet such as
that presented in Table 8.2. Setting the calculations
out in this manner not only enables the
user to check all the data, but also shows how each
variable contributes to the overall factor of safety.
Hence, if it is required to check the influence of the
cohesion on both planes falling to zero, this can be
done by setting the two groups containing the
cohesion values cA and cB to zero, giving a factor of
safety of 0.62.
18. Alternatively, the effect of drainage can be checked by varying the water density to simulate the effect of reducing the
water pressure. In this example, with cohesive strength, the factor is 1.98 when the slope is completely drained, and the
factor of safety is 1.24 for friction only, drained.
As has been emphasised in previous chapters, this ability to check the sensitivity of the factor of safety to changes in
material properties or water pressures is important because the value of these parameters is difficult to define precisely.
19.
20. 8.5 WEDGE STABILITY CHARTS FOR FRICTION ONLY
A rapid check of the stability of a wedge can be made if the slope is drained and cohesion is zero on both
slide planes A and B. Under these conditions, Equation 8.9 reduces to
(8.14)
The dimensionless factors A and B are found to depend upon the dips and dip directions of the two
planes. The values of these two factors have been computed for a range of wedge geometries, and the
results are presented as a series of charts (Figures 8.8 to 8.15).
Note that the factor of safety calculated from Equation 8.14 is independent of the slope height, the angle
of the slope face and the inclination of the upper slope surface. This rather surprising result arises
because the weight of the wedge occurs in both the numerator and denominator of the factor of safety
equation and, for the friction-only case, this term cancels out, leaving dimensionless ratios that define the
factor of safety. As discussed in Section 1.4, the factor of safety of a plane failure is also independent of
the slope dimensions if the slope is drained and the cohesion is zero. This simplification is very useful in
that it enables the user of these charts to carry out a quick check on the stability of a slope based on the
dips and dip directions of the two discontinuities that form the slide planes of the wedge. An example of
such an analysis is presented later in this chapter.
21. Many trial calculations have shown that a wedge having a factor of safety in excess of 2.0, as obtained
from the friction-only stability charts, is unlikely to fail under even the most severe combination of
conditions to which the slope is likely to be subjected. Consider the example discussed in Section 8.4 in
which the factor of safety for the worst conditions (zero cohesion and maximum water pressure) is 0.62.
This is 50% of the factor of safety of 1.24 for the friction-only case. Hence, had the factor of safety for
the friction-only case been 2.0, the factor of safety for the worst conditions would have been 1.0,
assuming that the ratio of the factors of safety for the two cases remains constant.
On the basis of such trial calculations, it is suggested that the friction-only stability charts can be used to
define those slopes that are adequately stable and can be ignored in subsequent analyses, that is,
slopes having a factor of safety in excess of 2.0. Slopes with a factor of safety, based upon friction only,
of less than 2.0 must be regarded as potentially unstable and require further detailed examination as
discussed in Section 8.6 and Appendix III.
In the design of the cut slopes on many projects, it will be found that these friction-only stability charts
provide all the information that is required for preliminary design and planning stages of a slope project.
This information will help identify potentially unstable wedges before excavation of the slope is started.
During construction, the charts can be used to make a rapid check of stability conditions when, for
example, faces are being mapped as the excavation is proceeding and decisions are required on the
need for support. If the factor of safety is less than 2.0, the detailed analysis can be used to design a
bolting pattern (see Appendix III).
22. Figure 8.8 Wedge stability charts for friction only: A and B charts
for a dip difference of 0°. Note: The flatter of the two planes is
always called plane A.
23. Figure 8.9 Wedge stability charts for friction only: A and B charts for a dip difference of 10°.
24. Figure 8.10 Wedge stability charts for friction only: A and B charts for a dip difference of 20°.
25. Figure 8.11 Wedge stability charts for friction only: A and B charts for a dip difference of 30°.
26. Figure 8.12 Wedge stability charts for friction only: A and B charts for a dip difference of 40°.
27. Figure 8.13 Wedge stability charts for friction only: A and B charts for a dip difference of 50°.
28. Figure 8.14 Wedge stability charts for friction only: A and B charts for a dip difference of 60°.
29. Figure 8.15 Wedge stability charts for friction only: A and B charts for a dip difference of 70°.
30. The following example illustrates the use of the friction-only charts, in which plane A has the flatter dip
(Table 8.3).
The first step in the analysis is to calculate the absolute values of the difference in the dip angles, and the
difference in the dip direction angles (third line in Table 8.3). For a dip difference of 30°, the values of
ratios A and B are determined from the two charts in Figure 8.11 for a difference in dip direction of 120°.
The values of A and B are 1.5 and 0.7, respectively, and substitution in Equation 8.14 gives the factor of
safety of 1.30. The values of A and B give a direct indication of the contribution which each of the planes
makes to the total factor of safety.
31. Figure 8.11 Wedge stability charts for friction only: A and B charts for a dip difference of 30°.
32. 8.5.1 Example of wedge analysis using friction-only charts
During the route location study for a proposed highway, the layout engineer has requested guidance on
the maximum safe angles that may be used for the design of the slopes. Extensive geological mapping of
outcrops, together with core logging, identified five sets of discontinuities in the rock mass through which
the road will pass. The dips and dip directions of these discontinuities are shown in Table 8.4, together
with the measured variation in these measurements.
Note that, because the mapping covers the entire alignment that extends over several kilometres, the
scatter in the dip and dip direction measurements can be taken into account in the analysis.
33. Figure 8.16 shows the pole locations for these five sets
of discontinuities (inverted triangle). Also shown in this
figure are the extent of the scatter in the pole
measurements, and the great circles corresponding to
the average pole positions. The dashed figure
surrounding the great circle intersections is obtained by
rotating the stereoplot to find the extent to which the
intersection point is influenced by the scatter around the
pole points. The intersection of great circles 2 and 5 has
been excluded from the dashed figure because it
defines a line of intersection dipping flatter than 20°,
which is less than the estimated angle of friction.
Figure 8.16 Stereoplot of geological data for preliminary design of
highway slopes. Black triangles mark most likely position of poles of five
sets of discontinuities present in rock mass; shaded area surrounding
pole position defines extent of scatter in measurements; factors of
safety for each combination of discontinuities are shown in circle over
corresponding intersection of great circles; dashed line surrounds area
of potential instability (FS < 2).
34. The factors of safety for each of the discontinuity intersections are determined from the wedge
charts, assuming a friction angle of 30° (some interpolation is necessary), and the values are
given in the circles over the intersection points. Because all of the planes are steep, some of
the factors of safety are dangerously low. Since it is likely that slopes with a factor of safety of
less than 1.0 will fail as the slope is excavated, the only practical solution is to cut the slopes at
an angle that is coincident with the dip of the line of intersection. For marginally stable wedges
with factors of safety between 1.0 and 2.0, a detailed analysis can be carried out to determine
the bolting force required to increase the factor of safety to an acceptable level.
The stereoplot in Figure 8.16 can be used to find the maximum safe slope angle for the slopes
of any dip direction. This stereographic analysis involves positioning the great circle
representing the slope face for a particular dip direction in such a way that the unstable region
(shaded) is avoided. The maximum safe slope angles are marked around the perimeter of this
figure and their positions correspond to the orientation of the slope face (Figure 8.17a). For
example, if a through cut for a highway is planned in this rock, the slope on the south side of the
cut would be an angle of 30° and the slope on the north side would be at 85° (Figure 8.17b).
35. Figure 8.17 Slope design based on wedge stability analysis: (a) stereoplot of great circles representing stable slopes in a rock
mass containing the five sets of discontinuities defined in Figure 8.16; (b) stable cut slopes angles based on wedge stability
analysis shown in (a).
36. 8.6 COMPREHENSIVE WEDGE ANALYSIS
8.6.1 Data for comprehensive analysis
If the friction-only wedge stability charts show that the factor of safety is less than 2.0, then a comprehensive stability
analysis may be required to calculate, for example, the bolting force to achieve a required factor of safety. This analysis
takes into account the dimensions and shape of the wedge, different cohesion and friction angles on each slide plane,
water pressure and a number of external forces. The external forces that may act on the wedge include earthquake
ground motion, tensioned bolts and possible loads generated by structures that may include a bridge foundation or
building located on the wedge.
Figure 8.18 shows the features of the slope involved in the comprehensive wedge analysis, and a complete list of the
equations used in the analysis is included in Appendix III. A fundamental assumption in the analysis is that all the forces
act through the centre of gravity of the wedge and so no moments are generated. The following is a description of the
components of the analysis:
1. Wedge shape – the shape of the wedge is defined by five surfaces: the two slide planes (1 and 2) with their line of
intersection daylighting in the face, the upper slope (3) and face (4), and a tension crack (5) (Figure 8.18a). The
orientations of these surfaces are each defined by their dips and dip directions. The range of orientations that the
analysis can accommodate include an overhanging face, different dip directions for the upper slope and the face,
and a tension crack dipping either towards or away from the face.
2. Wedge dimensions – the dimensions of the wedge are defined by the two dimensions H1 and L (Figure 8.18a). H1 is
the vertical height between the point where the line of intersection daylights on the face and the intersection of plane
1 with the crest of the slope, L is the distance measured along plane 1 between the crest of the slope face (4) and
the tension crack (5).
37. Figure 8.18 Comprehensive wedge analysis: (a) dimensions and surfaces defining size and shape of wedge; (b) water pressures
acting in tension crack and along the line of intersection; (c) optimum anchor orientation for reinforcement of a
wedge.
38. 3. Wedge weight – the orientations of the five planes, and the two dimensions can be used to calculate the volume of the
wedge, and the weight is determined from the unit weight of the rock (gr).
4. Water pressures – if it is assumed that the tension crack (5) is filled with water and that the water discharges to the
atmosphere where planes 1 and 2 intersect the face (plane 4), then triangular water pressures act on planes 1, 2 and
5 (Figure 8.18b). The water pressure p at the base of the tension crack (and the top of the line of intersection) is equal
to (h5 · gw), where h5 is the average vertical depth below the top of the tension crack. The water forces U1, U2 and V
are calculated by integrating the pressures over the areas of planes 1, 2 and 5, respectively.
In the analysis, the effect of slope drainage is simulated by reducing the unit weight of the water to less than
9.81 kN/m3 (62.5 lb/ft3). This approach simplifies the calculation of areas of the saturated portions of the planes 2, 3
and 5, and was a convenience when the calculations were being carried out by hand.
5. Shear strengths – the slide planes (1 and 2) can have different shear strengths defined by the cohesion (c) and friction
angle (ϕ). The shear resistance is calculated by multiplying the cohesion by the area of slide plane, and adding the
product of the effective normal stress and the friction angle. The normal stresses are found by resolving the wedge
weight in directions normal to each slide plane (see Equations 8.3 to 8.5).
6. External forces – external forces acting on the wedge are defined by their magnitude and orientation (plunge ψ, and
trend α). The equations listed in Appendix III can accommodate a total of two external forces; if three or more forces
are acting, the vectors are added as necessary. One external force that may be included in the analysis is the pseudo-
static force used to simulate seismic ground motion (see Section 11.6). The horizontal component of this force would
act in the same direction as the line of intersection of planes 1 and 2.
7. Bolting forces – if tensioned anchors are installed to stabilise the wedge, they are considered to be an external force.
Note that the calculated bolting force is the required force to support the entire wedge, in comparison to plane failure
where all forces are calculated per linear metre of slope.
39. The orientation of the anchors can be optimised to minimise the anchor force required to produce a specified factor of
safety. The optimum anchor plunge yT(opt) and trend aT(opt), with respect to the line of intersection (yi/ai), are as
follows (Figure 8.18c):
and
(8.15) (8.16)
where ϕaverage is the average friction angle of the two slide planes.
8.6.2 Computer programs for comprehensive analysis
Appendix III lists equations that can be used to carry out a comprehensive stability analysis of a wedge using the input
parameters discussed in Section 8.6.1. These equations were originally developed by Dr. John Bray and were included
in the third edition of Rock Slope Engineering (1981). This method of analysis has been used in a number of computer
programs that allow rapid and reliable analysis of wedge stability. However, the following limitation to this analysis
should be noted.
Wedge geometry – the analysis procedure is to calculate the dimensions of a wedge that extends from the face to the
point where planes 1, 2 and 3 intersect. The next step is to calculate the dimensions of a second wedge formed by
sliding planes 1 and 2, the upper slope (plane 3) and the tension crack (plane 5). The dimensions of the wedge in front
of the tension crack are then found by subtracting the dimensions of the wedge in front of the tension crack from the
overall wedge (see Equations III.54 to III.57, Appendix III). Prior to performing the subtractions, the programme tests to
see whether a wedge is formed and a tension crack is valid (Equations III.48 to III.53, Appendix III). The programme will
terminate if the dip of the upper slope (plane 3) is greater than the dip of the line of intersection of planes 1 and 2, or if
the tension crack is beyond the point where planes 1, 2 and 3 intersect.
40. While these tests are mathematically valid, they do not allow for a common geometric condition that may exist in steep
mountainous terrain. That is, if plane 3 is steeper than the line of intersection of planes 1 and 2, a wedge made up of
five planes can still be formed if a tension crack is located behind the slope face to create a valid plane 5. Where this
physical condition exists in the field, an alternative method of analysis is to use key block theory in which the shape and
stability condition of removal wedges can be completely defined (Goodman and Shi, 1985; PanTechnica Corporation,
2002) or other commercial programmes (Rocscience Inc).
8.6.3 Example of comprehensive wedge analysis
The following is an example of the comprehensive stability analysis of a wedge using the programme Swedge
(Rocscience Inc). Consider the wedge formed by joint sets 3 and 5 in Figure 8.16. This has a friction-only factor of
safety of 1.0, so water pressures and seismic ground motion may result in instability, depending on the cohesions on
the slide surfaces.
This analysis shows the bolting force required to raise the factor of safety to 1.5, based on the input parameters shown
in Table 8.5.
The other input parameters are as follows:
Wedge height, H1 = 28 m
Distance of tension crack from crest measured along plane 3, L = 15 m
Rock density, gr = 26 kN/m3 (62.5 lb/ft3)
Water density, gw = 9.81 kN/m3 (165 lb/ft3)
Seismic coefficient (horizontal), kH = 0.1 · g
41. This wedge has a line of intersection of 38° (plunge) and 063° (trend). This plunge angle is greater than the friction
angle of either sliding surface and so sliding of the wedge is possible. The weight of the wedge is 121.3 MN, which
indicates the magnitude of the bolting force that is required to significantly improve the factor of safety.
The stability analysis of the wedge using these parameters gave the following results:
1. Dry, static, c1 = c2 = 0, T = 0 FS = 1.05
Case (1) corresponds to the simplified analysis using the friction-only charts for a dry, static slope that gives a factor
of safety of 1.05.
2. zw = 50%, static, c1 = c2 = 0, T = 0 FS = 0.97
Case (2) shows that for the friction-only condition and the tension crack half filled with water, the factor of safety
reduces from 1.05 to 0.97.
3. zw = 50%, static, c1 = 50 kPa (7.3 psi), c2 = 0, T = 0 FS = 1.24
Case (3) shows that the effect of the cohesion of only 50 kPa (7.3 psi) acting on the 491 m2 area of plane 1 is to
increase the factor of safety to 1.24.
4. zw = 50%, kH = 0.1 · g, c1 = 50 kPa (7.3 psi), c2 = 0, T = 0 FS = 1.03
42. 4. zw = 50%, kH = 0.1 · g, c1 = 50 kPa (7.3 psi), c2 = 0, T = 0 FS = 1.03
Case (4) shows that the effect of a pseudo-static force kH = 0.1 · g for the same water pressure (zw = 50%) is to
reduce the factor of safety from 1.24 to 1.03.
5. T = 24,000 kN, aT = 243°, yT = −8°, zw = 50%, kH = 0.1 · g, c1 = 50 kPa (7.3 psi), c2 = 0 FS = 1.50
Case (5) shows that if tensioned bolts with a capacity of 24,000 kN (5400 kips) are installed at the optimum angle as
defined by Equations 8.15 and 8.16, that is, parallel to line of intersection and 8° above the horizontal, the factor of
safety is increased to 1.5.
6. T = 25,500 kN, aT = 249°, yT = +10°, zw = 50%, kH = 0.1 · g, c1 = 50 kPa (7.3 psi), c2 = 0 FS = 1.50
Case (6) shows that if the bolts are installed at right angles to the face and at a plunge angle of 10° below the
horizontal to facilitate grouting, then the bolting force has to be increased from 24,000 kN to 25,500 kN (5732 kips) for
the factor of safety to be the same as that for the bolts installed at the optimum orientation.