Limit-Equilibrium Stability Analysis of Spiling Soil Reinforcement in Tunneling

Size: px
Start display at page:

Download "Limit-Equilibrium Stability Analysis of Spiling Soil Reinforcement in Tunneling"

Transcription

1 58 Transportation Research Record 18 Limit-Eqilibrim Stability Analysis of Spiling Soil Reinforcement in Tnneling S. BANG ABSTRACT A limit-analysis procedre for a spiling reinforcement system in soft-grond tnneling is described. The system is composed of a series of radially installed reinforcing spiles along the perimeter of the tnnel opening before excavation. The reinforcing spile network is extended into the in sit mass both radially and longitdinally, The system ths forms a temporary spport with the advantage of not loosening the weak mass. It has been sccessflly sed in weak rock formations as well as in soft grond on limited occasions. The limitanalysis formlation incldes consideration of design parameters sch as soil type and geometry of the tnnel and the reinforcing spiles. The procedre developed can be sed to evalate the overall stability or to determine the design parameters of the system or both. In recent years ndergrond constrction has increased considerably as a logical part of the soltion to many rban problems. Effective and safe ndergrond excavation technology therefore has been soght to meet the challenge of this increasing demand. On several occasions a spiling reinforcement system has been sccessflly sed in tnneling to strengthen weak rock formations (1), On limited occasions the application also involved reinforcing tnnels in soft grond. The system typically consists of a series of radially installed reinforcing spiles 4.6 to 6.1 m long spaced between.6 and 1.5 m with an inclination angle of approximately 3 degrees to the tnnel axis. The reinforcing spiles are formed by inserting 2.5- to 3.B-cm diameter rebacs into predrilled holes with sbseqent grot. Figre 1 is a schematic representation of the system, the general principle of which is to stabilize a weak mass by installing an annlar spiling reinforcement network along the perimeter of the tnnel heading before excavation. The reinforcing network is extended into the in sit mass both radially and longitdinally. The tnneling operation is therefore always performed inside a tblar reinforced zone encircling the tnnel opening. Spile Set FIGURE I Spiling reinforcement system. A limit-analysis procedre for the spiling reinforcement system in soft-grond tnneling is presented. The formlation incldes consideration of design parameters sch as soil type, depth and diameter of the tnnel, and length, inclination, and spacing of the spiles. The analysis procedre can be sed to evalate the overall stability of the system and to determine the proper size, spacing, and length of the spiles for a given site condition. BACKGROUND The principle of the spiling reinforcement system is to strengthen the weak mass srronding the tnnel excavation. The prpose is to improve the grond in terms of stand-p time by preventing loosening ( immediate stabilization) and to contribte to permanent stabilization of the tnnel opening by restricting deformation. Korbin and Brekke () condcted small-scale laboratory model tests to investigate the mechanism of spiling reinforcement in weak-rock tnneling. Behavior of cylindrical models with and withot spiling reinforcement nder niform external pressres was examined. The stdy indicates that the system can stabilize a weak rock mass effectively by redcing deformations and thereby deterioration de to strain softening, providing increased available strength, and maintaining arching action, which allows for increased tangential stress in the immediate vicinity of the opening. Field instrmentation was also implemented at two sites (3), The investigation was designed to address qli' estions related primarily to the magnitde, distribtion, and time history of the deformation-indced tension and bending of the spiles as a reslt of excavation. Deformation-indced tension was fond to be the major mechanism of the spiling reinforcement. A generalized plane strain finite-element method of analysis was developed to investigate the be- 1\avior of the spiling reinforcement system in soft grond (.!l. The method of analysis developed was sed to compare the reslts of the model tests condcted by Korbin and Brekke and was fond very effective (.?_). The generalized plane strain condition assmes three nonzero displacement components, none of which is dependent on the ot-of-plane coordinate; ths the ot-of-plane strain remains zero instead of the ot-of-plane displacement, as is commonly the case in the conventional plane strain approach. The main advantage of this approach is that it calclates three-dimensional stresses and

2 Bang 59 displacements, as the finite-element grid remains in two dimensions. A comprehensive parametric stdy to identify the effects of the varios design parameters of the syst.em was also condcted (6) by sing the developed generalized plane strai;- f i nite-element method of analysis. LIMIT ANALYSIS AT EQUILIBRIUM To date there have been no prototype failre stdies of this system. Indirect methods therefore mst be sed to approximate the failre mechanism. As shown in Figre 2, contors of maximm shear strains were obtained from the previosly described generalized plane strain finite-element analysis <!> and ths a potential failre srface can be approximated. The potential failre srface passes more or less throgh the side wall of the tnnel opening and propagates pward to form a crved srface. In this analysis the crved failre srface is approximated by two planes, defined by angles a 1 and a 2, with a change in direction at the back face of the reinforced zone as shown in Figre 2. A potential failre srface can then be determined by finding a set of angles al and a2 that yields the lowest overall factor of safety. Note that it is always assmed that a 1.S. a 2.S. 9 degrees. Formlation Figre 3 shows the free-body diagrams of the assmed failre wedge. Becase of the symmetry, only half of the failre wedge is considered. Forces acting on element 1 are w 1, Ni, S1, Q1, N3 and s 3 : W 1 =rh 3 2 cota 2 N 1 =rka H3 2 S1 =/JN1 w body weight, Pot en tiol Failre Srface From Finite Element Analysis Appro1dmoted Failre Maximm Shear Strain Contor (xl- 4 ) (!) 2 1 IT, rl' -- r2 UL, //::_":). s N Ka ' ' -- / a, 2 L2 ELEMENT 2 N1 S1 (',:-f t r ELEMENT I FIGURE 3 Free-body diagrams of failre wedge. tangential force, normal force, and active earth pressre coefficient. H2 _J_ The coefficient e describes the ratio between S1 and N1. Normal and tangential forces (N3 and s 3 ) can be obtained from the eqilibrim: N3 = (W S1) cose<2 + N1 sina2 Q is the srcharge. The coefficient e can be obtained, on the assmption that the developed resisting force along the assmed failre srface is eqal to the driving forcei that is, S3 = C' (HJ/sina2) +NJ tan</>' =(W1 +1 +Si)sina2 -N1 cosa2 (3) C' is the developed cohesion and qi' is the developed friction angle. Sbstitting Eqations 1 and 2 into Eqation 3 yields /J=2{CW1 +1)sina2 2 -N1 cosa2 sina2 -C'HJ - [(W1+1) cos<>2 + N1 sina2] tanr/>'sina2} 7 Ka 'Y HJ 2 ( cosa2 tan</>' - sina2) sin<>2 Forces W2 and N4 acting on Element 2 are W2 = r [H(r + L2 cosa1) - (rrr 2 /4) - (H2L2/2) cosa1] N4 = 1 /zko rh1 2 r = radis of tnnel, L2 length of failre srface of Element 2, and Ko at-rest earth pressre coefficient. Note that the normal force acting on the plane of symmetry (N4) is assmed to be the at-rest condition and that no shear force exists on the p lane of symmetry. Force eqilibrim of Element 2 yields (2) (4) (5) N1 = (W S1) cos<>1 - (N 1 -N 4 ) sina1 (6) Reinforced Reoion The driving forces of Elements 1 and 2 are s 3 and S2, respectively, as the developed resisting forces of Elements 1 and 2 are FIGURE 2 Potential failre srface from contors of maximm shear strains. SR 1 = C'L1 +NJ tan</>' SR2 =C'L2 +N2 tan</>'+ LTTT (7) n=l

3 6 Transportation Research Record 18 m N; "' N2 + })TN, n=l m ITTN = resltant of normal component of n=l spile force TT, resltant of tangential component of spile force TT, = component of developed spile axial force Tn on X-Y plane, Li = length of failre srface of element i, and m = nmber of all spiles that cross assmed failre srface. Figre 4 is the schematic representation of the spile force components.,resltant Forces in Spiles It is assmed in this formlation that the spiles have the same length, inclination angle, and spacing. Neglecting the bending and shear as observed in field instrmentation (1_), the maximm developed axial force in each spile (Tnl can be calclated. Denoting stress tensors on X-Y-Z space and space as g and g', respectively, axis l is directed along the individal spile axis, one can obtain direction matrix is defined as follows: (8) Zn is the depth to the middle of the effective length of the nth spile. Therefore normal stresses acting on the spile (cr 2 and 3) can be calclated from Eqations 8 and 9. The mean normal stress acting on the spile is then (IO) The reslting force in the spile is the developed frictional resistance; that is, diameter of spile, effective length of nth spile, spile spacing, spile cross section, and yield stress of spile. (ll) The vales of n and Zn can be obtained from the geometry (Figre 5) The projection of the nth spile on the X-Y plane forms an angle en with the Y-axis, From triangle OAB in Figre 5, it is obvios that Rn 2 = r 2 + Ll + 2 r Li cose<1 Becase Rn cosan = L 2 sina 1, one can obtain Rn= r [-B + (B 2-4A)y,/2A] (12) (13) (14) [ COSQ = slnacoson slna sfn8n - slnasin On cos a sinacos -sina cos 11] -SinaslnOn cos a A= (cosn/sine<i) 2 - I B = 2(cosn/tane<i) Angles a and an are defined in Figre 4. Stresses acting along the effective length of the spile (portion of the spile otside the failre wedge) can be assmed as Uy ='Y Zn (9) Therefore the effective length of the nth ( nl and the depth to the middle of the tive length (Znl can be calclatedi that is, Rn= -[(Rn - r)/sine<] Zn = H -[(Rn + R)/2] coson i is the length of the spile. spile ef fec- (15) 2 y ASSUMED FAILURE SURFACE ---,., '',, - -,,, T TTN' Tylin(a,+8n-9"1 Tn TycotC 1 + 8n-9o"l Ty Tn tin a a Spilt inclination an9lt mta1rtd lrom tnnel axi9 Bn Spi11 lncllnollon on X- Y plane m11red lrom Y Glll 3 x F1GURE 4 Forces in reinforcing spiles.

4 Bang 61 y Section 1-1 FIGURE 5 Geometric parameters. EVALUATION OF OVERALL STABILITY On the basis of Eqations 3, 6, and 7, the overall stability of the system can be analyzed. At any stage, the driving force and the developed resisting force mst be in eqilibrim; that is, 53 = SRl for Element 1 and 52 = 5R2 for Element 2, or S = 5Rl + 5R2 The overall factor of safety with respect to shear strength (FS) is defined as a factor of safety when FSc = FS = FS (2), FSc is the factor of safety with respect to cohesion and FS is the factor of safety with respect to friction. The factor of safety with respect to cohesion or friction is the ratio between the available cohesion or friction and the developed cohesion or friction; that is, C' = C/FSc and tan ' = tan /FS U.J f/) I, "T'"" , L = 1.5 D Spile Len9th 1,4 L = 1.25 D L = D f.'3 L=.75D a: 1.2 I.I Tnnel D iometer ( D) = 3.5 m Tnnel Depth (H) = m The overall factor of safety (FS) can then be determined. Becase the expressions for driving and resisting forces contain an nknown FS, direct soltion is not possible. An iteration method is therefore sed. A compter program was developed to calclate the overall factor of safety. For a given set of geometric and strength parameters, this program calclated the minimm overall factor of safety by searching a series of potential failre srfaces with different angles of al and a 2 Typical reslts of this limit-eqilibrim analysis are shown in Figre 6. The soil is silty clayey sand with an ndrained strength of c = kpa and = 33 degrees (8). The angle of spile inclination is 3 degrees to the tnnel axis in all cases. The reslts indicate that 1. The improvement in the factor of safety with respect to spile spacing is greater for longer spiles, and 2. The rate of increase in the factor of safety for a given spile length is greater for small spile spacings, as can be seen from the changes in slopes. Figres 7 and 8 show the affects of tnnel depth and length and spacing of the spiles on the factor of safety. It is interesting to note that for a given spile length and spacing the factor of safety SPILE SPACING (m) FIGURE 6 Typical reslts of limit analysis U.J Ill 1.6 Tnnel Diameter ( D) 3.5 m Spile Spocin9(s). 91 m Len9th (L) = 3.81 m a: L = 3.5 m 1.4 L = 2.29m L = I. 52m ' TUNNEL DEPTH ( m) FIGURE 7 Effects of tnnel depth and spile length on factor of safety.

5 62 Transportation Research Record Tnnel Diameter ( D) = 3 5 m UJ <[ CJ) a:: <[ Spile Length (L) = 3.5m Spile Spacing (s) =.61 m s=. 91m Potential Failre Srface From Finite Element Analysis Potential Failre Srface From Limit Analysis _... _. J TUNNEL DEPTH (m) F1GURE 8 Effects of tnnel depth and spile spacing on factor of safety. Tnnel Diameter= 3.5m Tnnel Depth= 6.1 m Spile Length = 2 29 m Spile Spacing=.91 m Splle Inclination= 3 Soil No. IC= kpa 4,, 33 y=l57n/m3 Reinforced Region decreases as tnnel depth increases ntil a critical depth is reached. The factor of safety increases slightly below the critical depth. The rate of the decreasing factor of safety above the critical depth is, however, mch greater than that of the increasing factor of safety below the critical depth. The critical depth is the location of the tnnel springline the sliding tendency of the assmed failre wedge is maximm. The analysis is based on the eqilibrim of driving and resisting forces along the assmed failre srfacei therefore the factor of safety indicates a ratio between available soil strength and reqired soil strength mobilization against the sliding. Indeed the sliding tendency wold be small at very shallow depths becase of the small overbrden and at greater depths becase of arching. DISCUSSION AND SUMMARY The stability analysis procedre of the spiling reinforcement system in soft-grond tnneling has been presented. A limiting stress eqilibrim analysis has been performed to establish a design method for the system. The potential failre srface is approximated by two planes, starting from the side of the tnnel with a transition at the interface between the reinforced and nreinforced regions. The parameters fond to be significant from the previos stdy are inclded in the formlation. Strength parameters, sch as cohesion and friction, are assmed to be only partially developed, nless failre is imminent. From the eqilibrim of the driving force and the developed resisting force, the overall factor of safety is obtained. A comparison of the pntent.ial failrp s11rf11r.p. predicted by the finite-element analysis with generalized plane strain conditions was made with that predicted by limiting stress eqilibrim analysis. Figre 9 shows one of the typical reslts. The agreement, thogh it has not yet been verified experimentally, between these two predicted crves is reasonably good. The proposed formlation for the design of the spiling reinforcement system in soft-grond tnneling is intended to inclde the most essential characteristics involved in the system. However, a great deal of additional research is needed to describe the behavior of the system completely. Frther research is necessary in areas sch as field instrmentation and model testing to verify the analytical reslts. F1GURE 9 Comparison of potential failre srfaces. ACKNOWLEDGMENT The research reported in this paper was spported by the.s. Department of Transportation. The athor is gratefl for this spport. REFERENCES 1. G.E. Korbin and T.L. Brekke. Model Stdy of Tnnel Reinforcement. Jornal of the Geotechnical Engineering Division, ASCE, Vol. 12, No. GT9, G.E. Korbin and T.L. Brekke. A Model Stdy of Spiling Reinforcement in Undergrond Openings. Technical Report MRD Missori River Division,.s. Army Corps of Engineers, G.E. Korbin and T.L. Brekke. Field Stdy of Tnnel Prereinforcement. Jornal of the Geotechnical Engineering Division, ASCE, Vol. 14, No. GT8, s. Bang. Analysis of a Spiling Reinforcement System in Soft Grond Tnneling. In Transportation Research Record 945, TRB, National Research Concil, Washington, D.C., 1984, pp s. Bang. Spiling Reinforcement System in Tnneling. Presented at 4th Astralia-New Zealand Conference on Geomechanics, Perth, Astralia, May s. Bang and C.K. Shen. Soil Reinforcement in Soft Grond Tnneling. Research Report DOT/RSPA/DNA- 5/83/5. U.S. Department of Transportation, Jan D.W. Taylor. Fndamentals of Soil Mechanics. John Wiley and Sons, Inc., New York, J.M. Dncan, P. Byrne, K.S. Wong, and P. Mabry. Strength, Stress-Strain and Blk Modls Parameters for Finite Element Analyses of Stresses and Movements in Soil Masses. Report UCB/GT/8-1. University of California, Berkeley, Ag Pblication of this paper sponsored by Committee on Sbsrface Soil-Strctre Interaction.

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University

Lecture Notes: Finite Element Analysis, J.E. Akin, Rice University 9. TRUSS ANALYSIS... 1 9.1 PLANAR TRUSS... 1 9. SPACE TRUSS... 11 9.3 SUMMARY... 1 9.4 EXERCISES... 15 9. Trss analysis 9.1 Planar trss: The differential eqation for the eqilibrim of an elastic bar (above)

More information

EVALUATION OF GROUND STRAIN FROM IN SITU DYNAMIC RESPONSE

EVALUATION OF GROUND STRAIN FROM IN SITU DYNAMIC RESPONSE 13 th World Conference on Earthqake Engineering Vancover, B.C., Canada Agst 1-6, 2004 Paper No. 3099 EVALUATION OF GROUND STRAIN FROM IN SITU DYNAMIC RESPONSE Ellen M. RATHJE 1, Wen-Jong CHANG 2, Kenneth

More information

1 Differential Equations for Solid Mechanics

1 Differential Equations for Solid Mechanics 1 Differential Eqations for Solid Mechanics Simple problems involving homogeneos stress states have been considered so far, wherein the stress is the same throghot the component nder std. An eception to

More information

3 2D Elastostatic Problems in Cartesian Coordinates

3 2D Elastostatic Problems in Cartesian Coordinates D lastostatic Problems in Cartesian Coordinates Two dimensional elastostatic problems are discssed in this Chapter, that is, static problems of either plane stress or plane strain. Cartesian coordinates

More information

Effects of Soil Spatial Variability on Bearing Capacity of Shallow Foundations

Effects of Soil Spatial Variability on Bearing Capacity of Shallow Foundations Geotechnical Safety and Risk V T. Schweckendiek et al. (Eds.) 2015 The athors and IOS Press. This article is pblished online with Open Access by IOS Press and distribted nder the terms of the Creative

More information

Prandl established a universal velocity profile for flow parallel to the bed given by

Prandl established a universal velocity profile for flow parallel to the bed given by EM 0--00 (Part VI) (g) The nderlayers shold be at least three thicknesses of the W 50 stone, bt never less than 0.3 m (Ahrens 98b). The thickness can be calclated sing Eqation VI-5-9 with a coefficient

More information

IMPROVED ANALYSIS OF BOLTED SHEAR CONNECTION UNDER ECCENTRIC LOADS

IMPROVED ANALYSIS OF BOLTED SHEAR CONNECTION UNDER ECCENTRIC LOADS Jornal of Marine Science and Technology, Vol. 5, No. 4, pp. 373-38 (17) 373 DOI: 1.6119/JMST-17-3-1 IMPROVED ANALYSIS OF BOLTED SHEAR ONNETION UNDER EENTRI LOADS Dng-Mya Le 1, heng-yen Liao, hien-hien

More information

UNCERTAINTY FOCUSED STRENGTH ANALYSIS MODEL

UNCERTAINTY FOCUSED STRENGTH ANALYSIS MODEL 8th International DAAAM Baltic Conference "INDUSTRIAL ENGINEERING - 19-1 April 01, Tallinn, Estonia UNCERTAINTY FOCUSED STRENGTH ANALYSIS MODEL Põdra, P. & Laaneots, R. Abstract: Strength analysis is a

More information

Chapter 1: Differential Form of Basic Equations

Chapter 1: Differential Form of Basic Equations MEG 74 Energ and Variational Methods in Mechanics I Brendan J. O Toole, Ph.D. Associate Professor of Mechanical Engineering Howard R. Hghes College of Engineering Universit of Nevada Las Vegas TBE B- (7)

More information

DEVELOPMENT OF COMPONENT EXPLOSIVE DAMAGE ASSESSMENT WORKBOOK (CEDAW)

DEVELOPMENT OF COMPONENT EXPLOSIVE DAMAGE ASSESSMENT WORKBOOK (CEDAW) Abstract DEVELOPMENT OF COMPONENT EXPLOSIVE DAMAGE ASSESSMENT WORKBOOK (CEDAW) Charles.J. Oswald, Ph.D., P.E. Dale.T. Nebda, P.E. This paper smmarizes the methods sed to develop the Component Explosive

More information

Calculations involving a single random variable (SRV)

Calculations involving a single random variable (SRV) Calclations involving a single random variable (SRV) Example of Bearing Capacity q φ = 0 µ σ c c = 100kN/m = 50kN/m ndrained shear strength parameters What is the relationship between the Factor of Safety

More information

DISPLACEMENT ANALYSIS OF SUBMARINE SLOPES USING ENHANCED NEWMARK METHOD

DISPLACEMENT ANALYSIS OF SUBMARINE SLOPES USING ENHANCED NEWMARK METHOD DISPLACEMENT ANALYSIS OF SUBMARINE SLOPES USING ENHANCED NEWMARK METHOD N. ZANGENEH and R. POPESCU Faclt of Engineering & Applied Science, Memorial Universit, St. John s, Newfondland, Canada A1B 3X5 Abstract

More information

PIPELINE MECHANICAL DAMAGE CHARACTERIZATION BY MULTIPLE MAGNETIZATION LEVEL DECOUPLING

PIPELINE MECHANICAL DAMAGE CHARACTERIZATION BY MULTIPLE MAGNETIZATION LEVEL DECOUPLING PIPELINE MECHANICAL DAMAGE CHARACTERIZATION BY MULTIPLE MAGNETIZATION LEVEL DECOUPLING INTRODUCTION Richard 1. Davis & 1. Brce Nestleroth Battelle 505 King Ave Colmbs, OH 40201 Mechanical damage, cased

More information

Prediction of Effective Asphalt Layer Temperature

Prediction of Effective Asphalt Layer Temperature TRANSPORTATION RESEARCH RECORD 1473 93 Prediction of Effective Asphalt Layer Temperatre EARL H. INGE, JR., AND Y. RICHARD KIM The most widely sed method for evalating deflection measrements for overlay

More information

FEA Solution Procedure

FEA Solution Procedure EA Soltion Procedre (demonstrated with a -D bar element problem) MAE 5 - inite Element Analysis Several slides from this set are adapted from B.S. Altan, Michigan Technological University EA Procedre for

More information

Chapter 2 Introduction to the Stiffness (Displacement) Method. The Stiffness (Displacement) Method

Chapter 2 Introduction to the Stiffness (Displacement) Method. The Stiffness (Displacement) Method CIVL 7/87 Chater - The Stiffness Method / Chater Introdction to the Stiffness (Dislacement) Method Learning Objectives To define the stiffness matrix To derive the stiffness matrix for a sring element

More information

Evaluation of the Fiberglass-Reinforced Plastics Interfacial Behavior by using Ultrasonic Wave Propagation Method

Evaluation of the Fiberglass-Reinforced Plastics Interfacial Behavior by using Ultrasonic Wave Propagation Method 17th World Conference on Nondestrctive Testing, 5-8 Oct 008, Shanghai, China Evalation of the Fiberglass-Reinforced Plastics Interfacial Behavior by sing Ultrasonic Wave Propagation Method Jnjie CHANG

More information

Simplified Identification Scheme for Structures on a Flexible Base

Simplified Identification Scheme for Structures on a Flexible Base Simplified Identification Scheme for Strctres on a Flexible Base L.M. Star California State University, Long Beach G. Mylonais University of Patras, Greece J.P. Stewart University of California, Los Angeles

More information

The spreading residue harmonic balance method for nonlinear vibration of an electrostatically actuated microbeam

The spreading residue harmonic balance method for nonlinear vibration of an electrostatically actuated microbeam J.L. Pan W.Y. Zh Nonlinear Sci. Lett. Vol.8 No. pp.- September The spreading reside harmonic balance method for nonlinear vibration of an electrostatically actated microbeam J. L. Pan W. Y. Zh * College

More information

Advanced topics in Finite Element Method 3D truss structures. Jerzy Podgórski

Advanced topics in Finite Element Method 3D truss structures. Jerzy Podgórski Advanced topics in Finite Element Method 3D trss strctres Jerzy Podgórski Introdction Althogh 3D trss strctres have been arond for a long time, they have been sed very rarely ntil now. They are difficlt

More information

FEA Solution Procedure

FEA Solution Procedure EA Soltion Procedre (demonstrated with a -D bar element problem) EA Procedre for Static Analysis. Prepare the E model a. discretize (mesh) the strctre b. prescribe loads c. prescribe spports. Perform calclations

More information

Localization in Undrained Deformation 1

Localization in Undrained Deformation 1 Localization in Undrained Deformation 1 J. W. Rdnicki Dept. of Civil and Env. Engn. and Dept. of Mech. Engn. Northwestern University Evanston, IL 6001-3109 John.Rdnicki@gmail.com Janary 7, 009 1 To appear

More information

CPT-based lateral displacement analysis using p-y method for offshore mono-piles in clays

CPT-based lateral displacement analysis using p-y method for offshore mono-piles in clays Geomechanics and Engineering, Vol. 7, No. 4 (2014) 000-000 DOI: http://dx.doi.org/10.12989/gae.2014.7.4.000 000 CPT-based lateral displacement analysis sing p-y method for offshore mono-piles in clays

More information

Pulses on a Struck String

Pulses on a Struck String 8.03 at ESG Spplemental Notes Plses on a Strck String These notes investigate specific eamples of transverse motion on a stretched string in cases where the string is at some time ndisplaced, bt with a

More information

APPLICATION OF MICROTREMOR MEASUREMENTS TO EARTHQUAKE ENGINEERING

APPLICATION OF MICROTREMOR MEASUREMENTS TO EARTHQUAKE ENGINEERING 170 APPLICATION OF MICROTREMOR MEASUREMENTS TO EARTHQUAKE ENGINEERING I. M. Parton* and P. W. Taylor* INTRODUCTION Two previos papers pblished in this Blletin (Refs 1, 2) described the methods developed

More information

Lateral Load Capacity of Piles

Lateral Load Capacity of Piles Lateral Load Capacity of Piles M. T. DAVSSON, Department of Civil Engineering, University of llinois, Urbana Pile fondations sally find resistance to lateral loads from (a) passive soil resistance on the

More information

Setting The K Value And Polarization Mode Of The Delta Undulator

Setting The K Value And Polarization Mode Of The Delta Undulator LCLS-TN-4- Setting The Vale And Polarization Mode Of The Delta Undlator Zachary Wolf, Heinz-Dieter Nhn SLAC September 4, 04 Abstract This note provides the details for setting the longitdinal positions

More information

Two-media boundary layer on a flat plate

Two-media boundary layer on a flat plate Two-media bondary layer on a flat plate Nikolay Ilyich Klyev, Asgat Gatyatovich Gimadiev, Yriy Alekseevich Krykov Samara State University, Samara,, Rssia Samara State Aerospace University named after academician

More information

Modeling of Substrate-Induced Anisotropy in Through-Plane Thermal Behavior of Polymeric Thin Films

Modeling of Substrate-Induced Anisotropy in Through-Plane Thermal Behavior of Polymeric Thin Films Modeling of Sbstrate-ndced Anisotropy in Throgh-Plane Thermal Behavior of Polymeric Thin Films JONC B. L,'** MARK C. ALLN,' THOMAS C. HODC,' SU ANN BDSTRUP,' and PAUL A. KOHL' 'School of lectrical and

More information

Sareban: Evaluation of Three Common Algorithms for Structure Active Control

Sareban: Evaluation of Three Common Algorithms for Structure Active Control Engineering, Technology & Applied Science Research Vol. 7, No. 3, 2017, 1638-1646 1638 Evalation of Three Common Algorithms for Strctre Active Control Mohammad Sareban Department of Civil Engineering Shahrood

More information

Second-Order Wave Equation

Second-Order Wave Equation Second-Order Wave Eqation A. Salih Department of Aerospace Engineering Indian Institte of Space Science and Technology, Thirvananthapram 3 December 016 1 Introdction The classical wave eqation is a second-order

More information

Technical Note. ODiSI-B Sensor Strain Gage Factor Uncertainty

Technical Note. ODiSI-B Sensor Strain Gage Factor Uncertainty Technical Note EN-FY160 Revision November 30, 016 ODiSI-B Sensor Strain Gage Factor Uncertainty Abstract Lna has pdated or strain sensor calibration tool to spport NIST-traceable measrements, to compte

More information

BEHAVIOUR OF LATERALLY LOADED RIGID PILES IN COHESIVE SOILS BASED ON KINEMATIC APPROACH

BEHAVIOUR OF LATERALLY LOADED RIGID PILES IN COHESIVE SOILS BASED ON KINEMATIC APPROACH LOWLAND TECHNOLOGY INTERNATIONAL Vol., No., 7-4, Jne 8 International Association of Lowland Technology (IALT), ISSN 344-9656 BEHAVIOUR OF LATERALLY LOADED RIGID PILES IN COHESIVE SOILS BASED ON KINEMATIC

More information

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION

MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION MODELLING OF TURBULENT ENERGY FLUX IN CANONICAL SHOCK-TURBULENCE INTERACTION Rssell Qadros, Krishnend Sinha Department of Aerospace Engineering Indian Institte of Technology Bombay Mmbai, India 476 Johan

More information

Verification Analysis of the Gravity Wall

Verification Analysis of the Gravity Wall Verification Manal no. Update 0/06 Verification Analysis of the Gravity Wall Progra File Gravity Wall Deo_v_en_0.gtz In this verification anal yo will find hand-ade verification analysis calclations of

More information

FEA Solution Procedure

FEA Solution Procedure EA Soltion rocedre (demonstrated with a -D bar element problem) MAE - inite Element Analysis Many slides from this set are originally from B.S. Altan, Michigan Technological U. EA rocedre for Static Analysis.

More information

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec

1 JAXA Special Pblication JAXA-SP-1-E Small-scale trblence affects flow fields arond a blff body and therefore it governs characteristics of cross-sec First International Symposim on Fltter and its Application, 1 11 IEXPERIMENTAL STUDY ON TURBULENCE PARTIAL SIMULATION FOR BLUFF BODY Hiroshi Katschi +1 and Hitoshi Yamada + +1 Yokohama National University,

More information

Flexure of Thick Simply Supported Beam Using Trigonometric Shear Deformation Theory

Flexure of Thick Simply Supported Beam Using Trigonometric Shear Deformation Theory International Jornal of Scientific and Research Pblications, Volme, Isse 11, November 1 1 ISSN 5-15 Flere of Thick Simply Spported Beam Using Trigonometric Shear Deformation Theory Ajay G. Dahake *, Dr.

More information

Research Article An Analytical Solution for Lateral Buckling Critical Load Calculation of Leaning-Type Arch Bridge

Research Article An Analytical Solution for Lateral Buckling Critical Load Calculation of Leaning-Type Arch Bridge Mathematical Problems in Engineering, Article ID 578473, 4 pages http://dx.doi.org/.55/24/578473 Research Article An Analytical Soltion for Lateral Bckling Critical Load Calclation of Leaning-Type Arch

More information

SOIL NON-LINEAR BEHAVIOR AND HYSTERETIC DAMPING IN THE SPRING-DASHPOT ANALOG

SOIL NON-LINEAR BEHAVIOR AND HYSTERETIC DAMPING IN THE SPRING-DASHPOT ANALOG SOIL NON-LINEAR BEHAVIOR AND HYSTERETIC DAMPING IN THE SPRING-DASHPOT ANALOG Nikolaos OROLOGOPOULOS 1 and Dimitrios LOUKIDIS 2 ABSTRACT This paper presents reslts from nmerical simlations of footing vibration

More information

Stability of structures FE-based stability analysis

Stability of structures FE-based stability analysis Stability of strctres FE-based stability analysis Non-linear geometry, example P A B P C P= D -P Non-Linear geometry, example - kinematics The strains may be written as: The lengths of the bar in ndeformed

More information

PhysicsAndMathsTutor.com

PhysicsAndMathsTutor.com . Two smooth niform spheres S and T have eqal radii. The mass of S is 0. kg and the mass of T is 0.6 kg. The spheres are moving on a smooth horizontal plane and collide obliqely. Immediately before the

More information

Design and Data Acquisition for Thermal Conductivity Matric Suction Sensors

Design and Data Acquisition for Thermal Conductivity Matric Suction Sensors 68 TRANSPORTATION RSARCH RCORD 1432 Design and Data Acqisition for Thermal Condctivity Matric Sction Sensors J. K.-M. GAN, D. G. FRDLUND, A. XING, AND W.-X. LI The principles behind sing the thermal condctivity

More information

Effects of modifications on the hydraulics of Denil fishways

Effects of modifications on the hydraulics of Denil fishways BOREAL ENVIRONMENT RESEARCH 5: 67 79 ISSN 1239-6095 Helsinki 28 March 2000 2000 Effects of modifications on the hydralics of Denil fishways Riitta Kamla 1) and Jan Bärthel 2) 1) Water Resorces and Environmental

More information

METHODOLOGY FOR EXPERIMENTALLY DETERMINING THE CHARACTERISTICS OF MEDIUM VOLTAGE ZINC OXIDE VARISTORS

METHODOLOGY FOR EXPERIMENTALLY DETERMINING THE CHARACTERISTICS OF MEDIUM VOLTAGE ZINC OXIDE VARISTORS Copyright 01 by ABCM Page 973 METHODOLOGY FO EXPEIMENTALLY DETEMINING THE CHAACTEISTICS OF MEDIUM VOLTAGE ZINC OXIDE VAISTOS Barbosa, F.A.T., fernandotpinamba@ig.com.br Orlando, A.F., afo@pc-rio.br Pontifical

More information

Solving a System of Equations

Solving a System of Equations Solving a System of Eqations Objectives Understand how to solve a system of eqations with: - Gass Elimination Method - LU Decomposition Method - Gass-Seidel Method - Jacobi Method A system of linear algebraic

More information

08.06 Shooting Method for Ordinary Differential Equations

08.06 Shooting Method for Ordinary Differential Equations 8.6 Shooting Method for Ordinary Differential Eqations After reading this chapter, yo shold be able to 1. learn the shooting method algorithm to solve bondary vale problems, and. apply shooting method

More information

Efficiency Increase and Input Power Decrease of Converted Prototype Pump Performance

Efficiency Increase and Input Power Decrease of Converted Prototype Pump Performance International Jornal of Flid Machinery and Systems DOI: http://dx.doi.org/10.593/ijfms.016.9.3.05 Vol. 9, No. 3, Jly-September 016 ISSN (Online): 188-9554 Original Paper Efficiency Increase and Inpt Power

More information

Computational Fluid Dynamics Simulation and Wind Tunnel Testing on Microlight Model

Computational Fluid Dynamics Simulation and Wind Tunnel Testing on Microlight Model Comptational Flid Dynamics Simlation and Wind Tnnel Testing on Microlight Model Iskandar Shah Bin Ishak Department of Aeronatics and Atomotive, Universiti Teknologi Malaysia T.M. Kit Universiti Teknologi

More information

Inertial Instability of Arbitrarily Meandering Currents Governed by the Eccentrically Cyclogeostrophic Equation

Inertial Instability of Arbitrarily Meandering Currents Governed by the Eccentrically Cyclogeostrophic Equation Jornal of Oceanography, Vol. 59, pp. 163 to 17, 3 Inertial Instability of Arbitrarily Meandering Crrents Governed by the Eccentrically Cyclogeostrophic Eqation HIDEO KAWAI* 131-81 Shibagahara, Kse, Joyo,

More information

Details of Check for Boundary Element Requirements

Details of Check for Boundary Element Requirements COMUTERS AND STRUCTURES, INC., BERKELEY, CALIFORNIA DECEMBER 2001 SHEAR WALL DESIGN UCB 97 Technical te Wall ier Bondary Elements This Technical te describes how the program considers the bondary element

More information

Formal Methods for Deriving Element Equations

Formal Methods for Deriving Element Equations Formal Methods for Deriving Element Eqations And the importance of Shape Fnctions Formal Methods In previos lectres we obtained a bar element s stiffness eqations sing the Direct Method to obtain eact

More information

Subcritical bifurcation to innitely many rotating waves. Arnd Scheel. Freie Universitat Berlin. Arnimallee Berlin, Germany

Subcritical bifurcation to innitely many rotating waves. Arnd Scheel. Freie Universitat Berlin. Arnimallee Berlin, Germany Sbcritical bifrcation to innitely many rotating waves Arnd Scheel Institt fr Mathematik I Freie Universitat Berlin Arnimallee 2-6 14195 Berlin, Germany 1 Abstract We consider the eqation 00 + 1 r 0 k2

More information

Elements of Coordinate System Transformations

Elements of Coordinate System Transformations B Elements of Coordinate System Transformations Coordinate system transformation is a powerfl tool for solving many geometrical and kinematic problems that pertain to the design of gear ctting tools and

More information

Principles of Minimum Cost Refining for Optimum Linerboard Strength

Principles of Minimum Cost Refining for Optimum Linerboard Strength Principles of Minimm Cost Refining for Optimm Linerboard Strength Thomas J. Urbanik and Jong Myong Won ABSTRACT The mechanical properties of paper at a single basis weight and a single targeted refining

More information

Curves - Foundation of Free-form Surfaces

Curves - Foundation of Free-form Surfaces Crves - Fondation of Free-form Srfaces Why Not Simply Use a Point Matrix to Represent a Crve? Storage isse and limited resoltion Comptation and transformation Difficlties in calclating the intersections

More information

MECHANICS OF SOLIDS COMPRESSION MEMBERS TUTORIAL 2 INTERMEDIATE AND SHORT COMPRESSION MEMBERS

MECHANICS OF SOLIDS COMPRESSION MEMBERS TUTORIAL 2 INTERMEDIATE AND SHORT COMPRESSION MEMBERS MECHANICS O SOIDS COMPRESSION MEMBERS TUTORIA INTERMEDIATE AND SHORT COMPRESSION MEMBERS Yo shold jdge yor progress by completing the self assessment exercises. On completion of this ttorial yo shold be

More information

FLUCTUATING WIND VELOCITY CHARACTERISTICS OF THE WAKE OF A CONICAL HILL THAT CAUSE LARGE HORIZONTAL RESPONSE OF A CANTILEVER MODEL

FLUCTUATING WIND VELOCITY CHARACTERISTICS OF THE WAKE OF A CONICAL HILL THAT CAUSE LARGE HORIZONTAL RESPONSE OF A CANTILEVER MODEL BBAA VI International Colloqim on: Blff Bodies Aerodynamics & Applications Milano, Italy, Jly, 2-24 28 FLUCTUATING WIND VELOCITY CHARACTERISTICS OF THE WAKE OF A CONICAL HILL THAT CAUSE LARGE HORIZONTAL

More information

Effect of Fracture Healing on Laboratoryto-Field

Effect of Fracture Healing on Laboratoryto-Field TRANSPORTATION RESEARCH RECORD 1286 173 Effect of Fractre Healing on Laboratoryto-Field Shift Factor ADLI AL-BALBISSI AND DALLAS N. LITTLE Laboratory fatige testing of asphalt co~crete can be sed t.o predict

More information

u P(t) = P(x,y) r v t=0 4/4/2006 Motion ( F.Robilliard) 1

u P(t) = P(x,y) r v t=0 4/4/2006 Motion ( F.Robilliard) 1 y g j P(t) P(,y) r t0 i 4/4/006 Motion ( F.Robilliard) 1 Motion: We stdy in detail three cases of motion: 1. Motion in one dimension with constant acceleration niform linear motion.. Motion in two dimensions

More information

FINITE ELEMENT MODELING OF EDDY CURRENT PROBES FOR EDGE EFFECT

FINITE ELEMENT MODELING OF EDDY CURRENT PROBES FOR EDGE EFFECT FIITE ELEMET MODELIG OF EDDY CURRET PROBES FOR EDGE EFFECT REDUCTIO Sarit Sharma, Ibrahim Elshafiey, Lalita Udpa, and Satish Udpa Department of Electrical and Compter Engineering Iowa State University

More information

Obliqe Projection. A body is projected from a point with different angles of projections 0 0, 35 0, 45 0, 60 0 with the horizontal bt with same initial speed. Their respective horizontal ranges are R,

More information

Consistent Numerical Model for Wind Buffeting Analysis of Long-Span Bridges

Consistent Numerical Model for Wind Buffeting Analysis of Long-Span Bridges Consistent Nmerical Model for Wind Bffeting Analysis of Long-pan Bridges Dorian JANJIC Technical Director TDV GesmbH Graz, Astria Heinz PIRCHER Director TDV GesmbH Graz, Astria mmary The bffeting analysis

More information

Theoretical and Experimental Implementation of DC Motor Nonlinear Controllers

Theoretical and Experimental Implementation of DC Motor Nonlinear Controllers Theoretical and Experimental Implementation of DC Motor Nonlinear Controllers D.R. Espinoza-Trejo and D.U. Campos-Delgado Facltad de Ingeniería, CIEP, UASLP, espinoza trejo dr@aslp.mx Facltad de Ciencias,

More information

International Journal of Physical and Mathematical Sciences journal homepage:

International Journal of Physical and Mathematical Sciences journal homepage: 64 International Jornal of Physical and Mathematical Sciences Vol 2, No 1 (2011) ISSN: 2010-1791 International Jornal of Physical and Mathematical Sciences jornal homepage: http://icoci.org/ijpms PRELIMINARY

More information

Optimal Control of a Heterogeneous Two Server System with Consideration for Power and Performance

Optimal Control of a Heterogeneous Two Server System with Consideration for Power and Performance Optimal Control of a Heterogeneos Two Server System with Consideration for Power and Performance by Jiazheng Li A thesis presented to the University of Waterloo in flfilment of the thesis reqirement for

More information

Study on the impulsive pressure of tank oscillating by force towards multiple degrees of freedom

Study on the impulsive pressure of tank oscillating by force towards multiple degrees of freedom EPJ Web of Conferences 80, 0034 (08) EFM 07 Stdy on the implsive pressre of tank oscillating by force towards mltiple degrees of freedom Shigeyki Hibi,* The ational Defense Academy, Department of Mechanical

More information

Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model

Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model 90 TRANSPORTATION RESEARCH RECORD 1317 Analysis of Crack Propagation in Asphalt Concrete Using Cohesive Crack Model YEOU-SHANG }ENQ AND }IA-DER PERNG A cohesive crack model, which is similar to the Dgdale

More information

1. Solve Problem 1.3-3(c) 2. Solve Problem 2.2-2(b)

1. Solve Problem 1.3-3(c) 2. Solve Problem 2.2-2(b) . Sole Problem.-(c). Sole Problem.-(b). A two dimensional trss shown in the figre is made of alminm with Yong s modls E = 8 GPa and failre stress Y = 5 MPa. Determine the minimm cross-sectional area of

More information

Classify by number of ports and examine the possible structures that result. Using only one-port elements, no more than two elements can be assembled.

Classify by number of ports and examine the possible structures that result. Using only one-port elements, no more than two elements can be assembled. Jnction elements in network models. Classify by nmber of ports and examine the possible strctres that reslt. Using only one-port elements, no more than two elements can be assembled. Combining two two-ports

More information

Homotopy Perturbation Method for Solving Linear Boundary Value Problems

Homotopy Perturbation Method for Solving Linear Boundary Value Problems International Jornal of Crrent Engineering and Technolog E-ISSN 2277 4106, P-ISSN 2347 5161 2016 INPRESSCO, All Rights Reserved Available at http://inpressco.com/categor/ijcet Research Article Homotop

More information

arxiv: v1 [physics.flu-dyn] 11 Mar 2011

arxiv: v1 [physics.flu-dyn] 11 Mar 2011 arxiv:1103.45v1 [physics.fl-dyn 11 Mar 011 Interaction of a magnetic dipole with a slowly moving electrically condcting plate Evgeny V. Votyakov Comptational Science Laboratory UCY-CompSci, Department

More information

EXERCISES WAVE EQUATION. In Problems 1 and 2 solve the heat equation (1) subject to the given conditions. Assume a rod of length L.

EXERCISES WAVE EQUATION. In Problems 1 and 2 solve the heat equation (1) subject to the given conditions. Assume a rod of length L. .4 WAVE EQUATION 445 EXERCISES.3 In Problems and solve the heat eqation () sbject to the given conditions. Assme a rod of length.. (, t), (, t) (, ),, > >. (, t), (, t) (, ) ( ) 3. Find the temperatre

More information

4 Exact laminar boundary layer solutions

4 Exact laminar boundary layer solutions 4 Eact laminar bondary layer soltions 4.1 Bondary layer on a flat plate (Blasis 1908 In Sec. 3, we derived the bondary layer eqations for 2D incompressible flow of constant viscosity past a weakly crved

More information

The prediction of turbulence intensities in unsteady flow

The prediction of turbulence intensities in unsteady flow University of Wollongong Research Online Faclty of Engineering and Information Sciences - Papers: Part A Faclty of Engineering and Information Sciences 24 The prediction of trblence intensities in nsteady

More information

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB

Applying Laminar and Turbulent Flow and measuring Velocity Profile Using MATLAB IOS Jornal of Mathematics (IOS-JM) e-issn: 78-578, p-issn: 319-765X. Volme 13, Isse 6 Ver. II (Nov. - Dec. 17), PP 5-59 www.iosrjornals.org Applying Laminar and Trblent Flow and measring Velocity Profile

More information

UNIT V BOUNDARY LAYER INTRODUCTION

UNIT V BOUNDARY LAYER INTRODUCTION UNIT V BOUNDARY LAYER INTRODUCTION The variation of velocity from zero to free-stream velocity in the direction normal to the bondary takes place in a narrow region in the vicinity of solid bondary. This

More information

5. The Bernoulli Equation

5. The Bernoulli Equation 5. The Bernolli Eqation [This material relates predominantly to modles ELP034, ELP035] 5. Work and Energy 5. Bernolli s Eqation 5.3 An example of the se of Bernolli s eqation 5.4 Pressre head, velocity

More information

Motion in One Dimension. A body is moving with velocity 3ms towards East. After s its velocity becomes 4ms towards North. The average acceleration of the body is a) 7ms b) 7ms c) 5ms d) ms. A boy standing

More information

DEFINITION OF A NEW UO 2 F 2 DENSITY LAW FOR LOW- MODERATED SOLUTIONS (H/U < 20) AND CONSEQUENCES ON CRITICALITY SAFETY

DEFINITION OF A NEW UO 2 F 2 DENSITY LAW FOR LOW- MODERATED SOLUTIONS (H/U < 20) AND CONSEQUENCES ON CRITICALITY SAFETY DEFINITION OF A NEW UO 2 F 2 DENSITY LAW FOR LOW- MODERATED SOLUTIONS ( < 20) AND CONSEQUENCES ON CRITICALITY SAFETY N. Leclaire, S. Evo, I.R.S.N., France Introdction In criticality stdies, the blk density

More information

Regression Analysis of Octal Rings as Mechanical Force Transducers

Regression Analysis of Octal Rings as Mechanical Force Transducers Regression Analysis of Octal Rings as Mechanical Force Transdcers KHALED A. ABUHASEL* & ESSAM SOLIMAN** *Department of Mechanical Engineering College of Engineering, University of Bisha, Bisha, Kingdom

More information

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer

Chapter 6 Momentum Transfer in an External Laminar Boundary Layer 6. Similarit Soltions Chapter 6 Momentm Transfer in an Eternal Laminar Bondar Laer Consider a laminar incompressible bondar laer with constant properties. Assme the flow is stead and two-dimensional aligned

More information

Nonlinear parametric optimization using cylindrical algebraic decomposition

Nonlinear parametric optimization using cylindrical algebraic decomposition Proceedings of the 44th IEEE Conference on Decision and Control, and the Eropean Control Conference 2005 Seville, Spain, December 12-15, 2005 TC08.5 Nonlinear parametric optimization sing cylindrical algebraic

More information

1. INTRODUCTION. A solution for the dark matter mystery based on Euclidean relativity. Frédéric LASSIAILLE 2009 Page 1 14/05/2010. Frédéric LASSIAILLE

1. INTRODUCTION. A solution for the dark matter mystery based on Euclidean relativity. Frédéric LASSIAILLE 2009 Page 1 14/05/2010. Frédéric LASSIAILLE Frédéric LASSIAILLE 2009 Page 1 14/05/2010 Frédéric LASSIAILLE email: lmimi2003@hotmail.com http://lmi.chez-alice.fr/anglais A soltion for the dark matter mystery based on Eclidean relativity The stdy

More information

AN ISOGEOMETRIC SOLID-SHELL FORMULATION OF THE KOITER METHOD FOR BUCKLING AND INITIAL POST-BUCKLING ANALYSIS OF COMPOSITE SHELLS

AN ISOGEOMETRIC SOLID-SHELL FORMULATION OF THE KOITER METHOD FOR BUCKLING AND INITIAL POST-BUCKLING ANALYSIS OF COMPOSITE SHELLS th Eropean Conference on Comptational Mechanics (ECCM ) 7th Eropean Conference on Comptational Flid Dynamics (ECFD 7) 5 Jne 28, Glasgow, UK AN ISOGEOMETRIC SOLID-SHELL FORMULATION OF THE KOITER METHOD

More information

Department of Industrial Engineering Statistical Quality Control presented by Dr. Eng. Abed Schokry

Department of Industrial Engineering Statistical Quality Control presented by Dr. Eng. Abed Schokry Department of Indstrial Engineering Statistical Qality Control presented by Dr. Eng. Abed Schokry Department of Indstrial Engineering Statistical Qality Control C and U Chart presented by Dr. Eng. Abed

More information

PROBABILISTIC APPROACHES TO STABILITY AND DEFORMATION PROBLEMS IN BRACED EXCAVATION

PROBABILISTIC APPROACHES TO STABILITY AND DEFORMATION PROBLEMS IN BRACED EXCAVATION Clemson Uniersity TigerPrints All Dissertations Dissertations 12-2011 PROBABILISTIC APPROACHES TO STABILITY AND DEFORMATION PROBLEMS IN BRACED EXCAVATION Zhe Lo Clemson Uniersity, jerry8256@gmail.com Follow

More information

PROBLEMS

PROBLEMS PROBLEMS------------------------------------------------ - 7- Thermodynamic Variables and the Eqation of State 1. Compter (a) the nmber of moles and (b) the nmber of molecles in 1.00 cm of an ideal gas

More information

PREDICTABILITY OF SOLID STATE ZENER REFERENCES

PREDICTABILITY OF SOLID STATE ZENER REFERENCES PREDICTABILITY OF SOLID STATE ZENER REFERENCES David Deaver Flke Corporation PO Box 99 Everett, WA 986 45-446-6434 David.Deaver@Flke.com Abstract - With the advent of ISO/IEC 175 and the growth in laboratory

More information

Uncertainty Analysis of the Thunder Scientific Model 1200 Two-Pressure Humidity Generator

Uncertainty Analysis of the Thunder Scientific Model 1200 Two-Pressure Humidity Generator Uncertainty Analysis of the hnder cientific Model 100 wo-ressre Hmidity Generator 1.0 Introdction escribed here is the generated hmidity ncertainty analysis, following the Gidelines of NI and NL International

More information

FREQUENCY DOMAIN FLUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS

FREQUENCY DOMAIN FLUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS 7 TH INTERNATIONAL CONGRESS O THE AERONAUTICAL SCIENCES REQUENCY DOMAIN LUTTER SOLUTION TECHNIQUE USING COMPLEX MU-ANALYSIS Yingsong G, Zhichn Yang Northwestern Polytechnical University, Xi an, P. R. China,

More information

STATIC, STAGNATION, AND DYNAMIC PRESSURES

STATIC, STAGNATION, AND DYNAMIC PRESSURES STATIC, STAGNATION, AND DYNAMIC PRESSURES Bernolli eqation is g constant In this eqation is called static ressre, becase it is the ressre that wold be measred by an instrment that is static with resect

More information

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA. PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 13 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS EDEXCEL NATIONAL CERTIFICATE/DIPLOMA PRINCIPLES AND APPLICATIONS of FLUID MECHANICS UNIT 3 NQF LEVEL 3 OUTCOME 3 - HYDRODYNAMICS TUTORIAL - PIPE FLOW CONTENT Be able to determine the parameters of pipeline

More information

Similarity Solution for MHD Flow of Non-Newtonian Fluids

Similarity Solution for MHD Flow of Non-Newtonian Fluids P P P P IJISET - International Jornal of Innovative Science, Engineering & Technology, Vol. Isse 6, Jne 06 ISSN (Online) 48 7968 Impact Factor (05) - 4. Similarity Soltion for MHD Flow of Non-Newtonian

More information

A Fully-Neoclassical Finite-Orbit-Width Version. of the CQL3D Fokker-Planck code

A Fully-Neoclassical Finite-Orbit-Width Version. of the CQL3D Fokker-Planck code A Flly-Neoclassical Finite-Orbit-Width Version of the CQL3 Fokker-Planck code CompX eport: CompX-6- Jly, 6 Y. V. Petrov and. W. Harvey CompX, el Mar, CA 94, USA A Flly-Neoclassical Finite-Orbit-Width Version

More information

Numerical Study on Bouncing and Separation Collision Between Two Droplets Considering the Collision-Induced Breakup

Numerical Study on Bouncing and Separation Collision Between Two Droplets Considering the Collision-Induced Breakup Jornal of Mechanical Science and Technology (007) 585~59 Jornal of Mechanical Science and Technology Nmerical Stdy on Boncing and Separation Collision Between Two Droplets Considering the Collision-Indced

More information

Sources of Non Stationarity in the Semivariogram

Sources of Non Stationarity in the Semivariogram Sorces of Non Stationarity in the Semivariogram Migel A. Cba and Oy Leangthong Traditional ncertainty characterization techniqes sch as Simple Kriging or Seqential Gassian Simlation rely on stationary

More information

ON THE LIMITS OF THE BETZ S EFFICIENCY COEFFICIENT OF WIND TURBINES WITH THE HORIZONTALLY SHAFT

ON THE LIMITS OF THE BETZ S EFFICIENCY COEFFICIENT OF WIND TURBINES WITH THE HORIZONTALLY SHAFT ON THE LIMITS OF THE BETZ S EFFICIENCY COEFFICIENT OF WIND TURBINES WITH THE HORIZONTALLY SHAFT Prof.dr. ing. Petre Terzi SOCIETATEA PENTRU PROMOVAREA ENERGIILOR REGENERABILE, INEPUIZABILE SI NOI SPERIN

More information

Available online at ScienceDirect. Procedia Engineering 150 (2016 )

Available online at   ScienceDirect. Procedia Engineering 150 (2016 ) Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 150 (016 ) 635 640 International Conference on Indstrial Engineering, ICIE 016 Research of Dynamics of the Rotor with Three-film

More information

A Single Species in One Spatial Dimension

A Single Species in One Spatial Dimension Lectre 6 A Single Species in One Spatial Dimension Reading: Material similar to that in this section of the corse appears in Sections 1. and 13.5 of James D. Mrray (), Mathematical Biology I: An introction,

More information