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Quantification of Effects of Fly Ash Type on Concrete Early-Age Cracking

By Riding, Kyle A,Poole, Jonathan L,Schindler, Anton K,Juenger, Maria C G,Folliard, Kevin J
Publication: ACI Materials Journal
Date: Saturday, March 1 2008
HEADNOTE

The mechanisms that contribute to early-age cracking are complex. Determining the relative importance of each mechanism as well as the combined cracking potential for a given concrete material is essential for the concrete industry to construct structures with a long

service life. A method for quantifying the cracking risk of a concrete mixture is presented. The method involves testing for the concrete heat of hydration, setting time, free thermal and autogenous movement, restrained stress, and mechanical property development. The concrete uniaxial stress under restrained conditions is measured using a rigid cracking frame. This test setup was used to quantify the effects of using fly ash on the concrete cracking risk using four different fly ashes with varying calcium oxide contents. All fly ashes reduced the cracking risk because of the decrease in the heat of hydration of the cementitious materials and, to a lesser extent, the increased early-age creep.

Keywords: cracking; early-age creep; fly ash; mass concrete.

(ProQuest: ... denotes formulae omitted.)

INTRODUCTION

In recent years, the drive for rapid construction and durable concrete has led to the use of very-high-strength concrete with lower water-cementitious material ratios (w/cm) and higher cementitious contents. At the same time, the size of many concrete bridge members has increased for structural and aesthetic reasons. The increased member size and increased cement content used have drawn concern over the potential risk for thermal and autogenous shrinkage cracking in these members. The last thing that owners want to see is very durable concrete between the cracks when they expect a durable structure.

The causes of restrained concrete cracking can be very complex. The cracking risk is dependent on the structural design, proper materials selection, and good construction practices. The structural design must allow for a reasonable amount of expansion and contraction. The concrete mixture proportions must then be designed to limit the heat of hydration, drying shrinkage, and autogenous shrinkage to acceptable levels for the member. The contractor must then use good construction practices, placement rates, and proper curing that are specific to the type of materials used (for example, concrete with supplementary cementing materials [SCMs] may need extra curing time to prevent cracking).

The selection of concrete materials with a low cracking risk involves many interrelated factors. A comparison of the concrete stress development with the strength development can be used to determine the cracking risk of a mixture.1 The stress development is dependent on the volume change, elastic modulus development, and rate of creep. The temperature development, and hence thermal volume change of concrete, depends on the aggregate type used, fresh concrete temperature, cementitious materials used, chemical admixtures, member size and dimensions, and environmental conditions.2 The autogenous shrinkage development depends on the temperature, cementitious materials used, and w/cm.3,4 The rate of elastic modulus development versus the rate of volume change and location of volume change in the member will determine how much beneficial precompression is developed in the concrete at early ages.5 The creep rate depends on the stress level, the concrete age, the materials, the elastic modulus, and the temperature.6,7

This paper will focus on a battery of tests that, when performed, will allow the user to ascertain the volume change, creep behavior, and mechanical property development of different concrete mixtures. The results of these tests allow direct quantification of the cracking sensitivity of a specific mixture. The testing regime was then used to examine the effect of fly ash with varying calcium oxide (CaO) levels on concrete cracking sensitivity. The CaO level of the fly ash has been shown to be an indicator of its cementitious nature and, thus, the amount of heat liberated during hydration.8 The following are not well understood: the relative importance of reducing the heat of hydration as compared with the reduction in early-age strength, and the increase in creep and decrease in elastic modulus associated with the use of fly ash. The testing regime described in this paper presents a method of quantifying the benefits of each material property, which can then be used in a varying-restraint-induced stress analysis and modeling of the structure to determine the cracking risk.

RESEARCH SIGNIFICANCE

Early-age cracking in mass concrete bridge members has become a concern in recent years. Bridge member sizes have increased, increasing the risk of thermal cracking in many structures. Lower w/cm concretes have been used to produce denser, lower permeability concrete, whereas at the same time increase the risk of autogenous shrinkage. This paper outlines a battery of tests that together may be used to assess the early-age thermal and autogenous shrinkage cracking risk of a concrete mixture. The effects of fly ash CaO content are examined as an example of the usefulness of this method.

EXPERIMENTAL PROCEDURE

The testing procedure used for this study for each concrete mixture can be divided up into two phases: the hydration characterization phase and the mechanical response phase. In the hydration characterization phase, semi-adiabatic calorimetry is performed on the concrete mixture. The adiabatic heat generation curve parameters8 obtained for the mixtures are then used to simulate the temperature development of the mixture in a specific structural element, which are imposed on the tests conducted under phase two. Other researchers have performed cracking tests by simulating various-sized concrete members and boundary conditions.9-11 The center point of a simulated 1 m (39 in.) thick wall was chosen to allow for a large heat gain and, therefore, large differentiation between material behaviors. The temperature history of concrete in the simulated wall was calculated using a constant surface temperature to keep the calculations simple and allow for the simulation of normal, hot, or cold climates. The concrete fresh temperature can also be changed in the simulation to quantify the effects of concrete precooling on the mixture's cracking sensitivity. The advantage of this approach is that the configuration of the structural member and nature of the cementitious materials system will dictate the concrete temperature development in each test. This approach thus allows one to test the cracking sensitivity of the concrete under realistic conditions that the concrete may be exposed to during construction. The experiments reported in this paper were conducted with a fresh temperature and simulated wall surface temperature of 23 °C (73 °F).

The mechanical response of the concrete mixture is tested in phase two of the testing program. The second phase of testing used in this testing regime allows for the quantification of the concrete mechanical property development, free thermal dilation, autogenous shrinkage, and early-age creep response. Figure 1 summarizes the testing sequence used.

The concrete uniaxial stress under restrained conditions is measured using a rigid cracking frame.12 Figure 2 shows a drawing of the rigid cracking frame and a picture of the test setup. A 150 x 150 x 1250 mm (6 x 6 x 49 in.) concrete specimen is placed, consolidated, and cured in the rigid cracking frame. The formwork of the rigid cracking frame allows the temperature of the freshly placed concrete to be conditioned to simulate various structural elements. The temperature of the rigid cracking frame specimen is controlled using a programmable refrigerating/heating circulator that circulates a 50/50% mixture of water and ethylene glycol through copper pipes in the formwork and cracking frame crosshead. The circulator is controlled based on the temperature in the middle of the cracking frame measured using a Type T thermocouple. The temperature in the concrete crossheads is also measured using Type T thermocouples. Because the temperature in the concrete is actively controlled, the difference between the temperature in the specimen middle and crosshead is generally within 0.5 °C (0.9 °F). If the concrete specimen does not crack after 96 hours, it is cooled at a rate of 1 °C/hour (1.8 °F/hour) to induce cracking in the concrete and to directly measure the concrete tensile strength. The temperature at which the concrete cracks is referred to as the cracking temperature.5 The lower the cracking temperature is, the better the concrete mixture resistance to thermal cracking will be.5

The stress in the rigid cracking frame is monitored with strain gauges mounted on the 100 mm (4 in.) diameter restraining bars. The system is statically determinant, allowing for the calculation of the concrete stress from knowledge of the force in the very low coefficient of thermal expansion iron-nickel alloy steel bars. The force in the steel bars is calculated using the measured strain and the frame stiffness that is obtained through a calibration procedure. During the calibration procedure, a known axial load is applied to the frame while the steel bar strain is measured. The degree of restraint provided by the bars on the concrete can be calculated using Eq. (1)12

... (1)

where σ is the degree of restraint (%); Ec is the concrete elastic modulus (MPa); Ac is the concrete cross-sectional area (m2); E^sub s^is the restraining bar modulus (MPa); and A^sub s^is the restraining bars cross-sectional area (m2). The temperature of the bars at the location of the strain gauges is measured using a resistance temperature detector (RTD) probe. The thermal movement of the restraining bars also needs to be subtracted from the measured strain to calculate the actual stress-induced strain in the bars, as shown in Eq. (2)

ε^sub Tadj^ = ΔT^sub ib^ × α^sub ib^ × σ (2)

where ε^sub Tadj^ is the temperature-induced strain of the bar; ΔT^sub ib^ is the temperature change of the bar at the strain gauge (°C); and α^sub ib^ is the coefficient of thermal expansion of the bar (m/m/°C).

A free shrinkage frame has been developed to measure the free thermal and autogenous dilation of the concrete mixture. It is advantageous to use a direct measurement of the concrete free shrinkage to eliminate errors that may come from using a constant coefficient of thermal expansion or an assumed autogenous shrinkage development. Figure 3 shows a diagram and picture of the free shrinkage frame. The free shrinkage specimen dimensions are 150 x 150 x 520 mm (6 x 6 x 20.4 in.). The bottom bar is made of a very low coefficient of thermal expansion iron-nickel alloy, as well as the threaded rods that are embedded in the concrete. The threaded rod is screwed onto the linear potentiometer, which is then threaded onto a 25 x 25 mm (1 x 1 in.) plate that is embedded in the concrete. The threaded rod is greased to allow for reuse. Two layers of plastic are used between the concrete and the formwork, with a petroleum-based lubricant applied under each layer, to reduce friction between the specimen and the formwork as much as possible. The copper pipes in the free-shrinkage frame's formwork are connected in series with the cracking frame and circulator to ensure that the free shrinkage frame's temperature stays within approximately 1 °C (1.8 °F) of the temperature of the concrete in the rigid cracking frame. The temperature is recorded using two thermocouples. The free shrinkage is initialized and set to zero at initial setting as determined following ASTM C403,14 also using temperature-controlled specimens as will be described in the following. Special care should be taken to make sure that the plastic extends to the end of the specimen and folds up so that mortar does not get under the plastic and increase friction. The top surface is sealed with plastic and adhesive aluminum tape. The opening on the end plate is drilled larger than the rod to reduce friction between the rod and the plate when the rod moves. Grease is used to fill the remainder of the hole left by the threaded rod to prevent moisture loss. The hole in the top formwork was drilled larger than the thermocouples to ensure that no restraint is provided by the thermocouple probes. Silicone is used to seal the holes in the formwork where the thermocouples are inserted.

Twenty-four 100 x 200 mm (4 x 8 in.) concrete cylinders are match-cured to the cracking frame temperature for mechanical property testing, as shown in Fig. 4. The concrete cylinders are placed in an insulated water bath immediately after finishing. The temperature of the water bath is controlled to within approximately 1 °C (1.8 °F) of the rigid cracking frame temperature by another 28 L (1 ft3) capacity refrigerating/heating circulator. The cylinders are tested at 1/2, 1, 2, 3, 7, and 28 days for compressive strength, static modulus of elasticity,14 and splitting tensile strength. When a cylinder is removed from the water bath for testing, it is replaced with a dummy cylinder to maintain a constant water level. A water bath is also placed in series with the concrete cylinder water bath to hold specimens for testing the time of setting of concrete mixtures by penetration resistance in accordance with ASTM C403.15 When the match-cured time of setting specimens achieve initial set, the end plates in the free shrinkage rig are backed away from the concrete.

Early-age concrete creep analysis

The modulus of elasticity development, free thermal deformations, and autogenous deformation are used as inputs to predict the stress development of the concrete in the rigid cracking frame. The temperature distribution in the bar is also used to simulate the thermal movement of the bar with time and the corresponding change in the degree of restraint of the concrete. The temperature distribution in the bar may be approximated by using symmetry and the temperature distribution for a fin of circular cross section with an adiabatic end tip (this is the case for symmetry in the middle of the restraining bar because there would be no heat exchange in the middle of a symmetrical bar). Equations (3) through (6) show how the temperature distribution of a fin of uniform cross section with an adiabatic tip could be analytically simulated16

... (3)

θ = T - T^sub ∞^ (4)

θ^sub b^ = T^sub b^ - T^sub ∞^(5)

... (6)

where L is half the length of the rod (because symmetry is being exploited) (m); x is the distance along the rod from the cracking frame crosshead (m); T is the temperature in the rod at location x (°C); T^sub b^ is the temperature of the rod at the cracking frame crosshead (°C); T^sub ∞^ is the ambient temperature (°C); h is the convection coefficient (W/m2/°C); k is the rod thermal conductivity (W/m/°C); and r is the rod radius (m).

Once the elastic strain is calculated, the creep response can then be calculated using the principle of superposition.6 The calculated stresses after creep can then be compared with the measured stresses. A regression analysis is used to determine the creep parameters that provide the best fit of the measured stresses. The procedure for calculating the early-age creep parameters by fitting creep constants to the measured concrete stresses in the rigid cracking frame assumes that creep in compression and tension are equal. In this paper, the linear logarithmic model (LLM), as developed by Larson,17 is used to model the creep behavior. The method models the creep compliance as two linear functions on a log scale, as shown in Fig. 5. Equations (7) and (8) show the creep compliance using the LLM17

... (7)

... (8)

for i = 1, 2, where ΔJ is the increase in creep compliance (1/Pa); Δt^sub load^ is the time from application of the load (days); Δt^sub 0^ is the time of load application (days), Δt^sub 1^ is the time limit that transitions between short-term and long-term creep (days), ts is the apparent setting time (days); a^sub i^^sup max^, a^sub i^^sup min^, t^sub ai^, and n^sub ai^ are fit parameters. Each of these parameters are defined and explained in detail elsewhere.17

MATERIALS TESTED

A total of five different concrete mixtures were tested using the procedure outlined previously. A Type I cement was used in all concrete mixtures tested. A No. 57 gradation18 siliceous river gravel coarse aggregate and natural siliceous sand were used in all mixtures. The mixture proportions used in each test are shown in Table 1. Four different fly ashes with varying CaO content, two ASTM C618 Class F and two Class C fly ashes,19 were tested at a 20% replacement level by mass. The fly ash chemical composition and Blaine fineness are shown in Table 2. All mixtures were tested using a w/cm of 0.42. All mixtures contained 4 oz/cwt of ASTM Type A low-range water reducing admixture.20

RESULTS AND DISCUSSION

The semi-adiabatic test results for each mixture were used to simulate the temperature at the middle of a 1 m (39 in.) thick wall with a constant surface temperature of 23 °C (73 °F). Figure 6 shows the temperature measured in the middle of the cracking frame specimens and the resulting stress development. All of the concrete mixtures containing fly ash show a significant reduction in heat of hydration, with the Class F fly ashes showing the most decrease. The penetration resistance values measured from the match-cured setting test specimens are shown in Fig. 7. All fly ashes tested show a retardation in setting compared with the control. The Class F ashes may retard setting due to a dilution of portland cement concentration. Both Class C fly ashes retard setting more than the Class F fly ashes. FA3 shows more retardation than the other fly ashes tested. Previous researchers have shown that Class C fly ashes can have different setting behaviors than Class F ashes, but results are highly variable.21 The cracking behavior of mixtures with significantly delayed settings may be quite different than that of mixtures measured in this paper. More extensive testing and caution is recommended when using mixtures with very long setting times. The cracking frame results (refer to Fig. 6(b)) show that all of the fly ashes tested lowered restraint stresses and improved cracking resistance. The Class F fly ashes lowered the cracking temperature by an average of 7.5 °C (13.5 °F), whereas the Class C fly ashes lowered the cracking temperature by an average of 4.2 °C (7.6 °F). Figure 8 shows the best-fit concrete splitting tensile strength development curves. It is significant to note that the mixtures containing Class F fly ash show the slowest strength gain rate, but the best cracking resistance as measured by the time to cracking and cracking temperature. The measured modulus values for all the concrete mixtures show similar modulus developments with time, indicating that the lower heat of hydration and increased creep are more influential parameters in reducing cracking. The cracking resistance that is lost by the reduced tensile strength gain is more than made up by the lowered thermal strain (caused by the lowered heat of hydration) and increased creep. The stress-to-splitting tensile strength ratio development with time was the quickest for the control mixture, but the fly ash mixture's development was only slightly lower, as shown in Fig. 9. The free thermal and autogenous dilation results are shown in Fig. 10. The fly ash mixtures showed considerable less expansion early on, probably because of the lowered heat of hydration during the first few hours of hydration during which time the coefficient of thermal expansion is higher.22-24

Creep parameters were fit from the stress, free shrinkage, and modulus development data using the LLM.17 A good fit of the stress data was achieved by adjusting only the ta1 parameter, as shown in Table 3. The magnitude of a^sub 1^^sup max^, a^sub i^^sup min^, and a^sub 2^^sup max^ are as recommended by Larson.17 Figure 11 shows the decrease in the a1 (the slope of the first linear portion or short-term creep compliance) parameter with time. The creep compliance decreased faster with time in the concrete mixtures that had a higher heat of hydration. The Class F fly ashes showed higher early age creep, which helped contribute to the increased cracking resistance.

A numerical investigation into the relative importance of early-age creep on the stress history was performed. Thermal stresses in a simulated cracking frame were calculated for the five mixtures using the creep parameters calculated and found in Table 3, the measured modulus development (using an equivalent age), and the temperature history recorded from the control mixture. The calculated stresses are shown in Fig. 12. In general, the higher the a1 parameter is, the lower the early-age stresses will be. FA3 was an exception to this rule and had a lower early-age stress than FA4 even though the a1 parameter was lower. This occurred because FA3 had a delayed setting. All of the mixtures were predicted to have higher tensile stresses than the control because of less beneficial precompression due to the increased early-age creep, but similar later age creep. Temperature effects on modulus and creep may give different actual results than that modeled. These numerical computations are not meant to imply that concrete containing fly ash increases the risk of cracking, only to illustrate the impact of the decrease in thermal strains. This simple numerical case study does show that the biggest impact on cracking resistance from the use of fly ash is the decrease in thermal movement. More research is needed on concrete containing fly ash at lower w/cm to investigate its effect on autogenous shrinkage.

CONCLUSIONS

A method for calculating concrete early-age creep parameters and determining the concrete resistance to cracking was presented. All fly ashes tested lowered the early-age cracking risk of concrete. The concrete containing fly ash had a lower tensile strength development than the control mixture. This indicates that, given equal stress development, the concrete containing fly ash should crack sooner than the control mixture. The cracking tendency for concrete containing fly ash, however, was lower because the stresses were reduced by a lowered thermal strain (caused by a lowered heat of hydration) and increased early-age creep. In fact, the cracking tendency for concrete containing low calcium oxide fly ash was the lowest, even though its rate of tensile strength development was the slowest. It is the combined effect of creep, lower heat of hydration, modulus development, and tensile strength gain that defines the cracking risk. More testing needs to be performed on concrete containing fly ash at lower w/cm to investigate the effects of fly ash on autogenous shrinkage.

Further research is recommended to identify and quantify the effect of variables such as aggregate type, aggregate gradation, w/cm, cement type, SCM type, and placement temperature on the cracking sensitivity of concrete.

ACKNOWLEDGMENTS

The authors wish to express their gratitude to the Texas Department of Transportation through Project 0-4563 for funding this research. The advice and support of R. Browne and T. Yarbrough of the Texas Department of Transportation is greatly appreciated. The guidance and assistance of R. Springenschmid and E. Gierlinger to develop the cracking frame test setup are appreciated.

SIDEBAR

ACI Materials Journal, V. 105, No. 2, March-April 2008.

MS No. M-2006-443 received November 14, 2006, and reviewed under Institute publication policies. Copyright © 2008, American Concrete Institute. All rights reserved, including the making of copies unless permission is obtained from the copyright proprietors. Pertinent discussion including authors' closure, if any, will be published in the January- February 2009 ACI Materials Journal if the discussion is received by October 1, 2008.

REFERENCE

REFERENCES

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19. ASTM C618, "Standard Specification for Coal Fly Ash and Raw or Calcined Natural Pozzolan for Use in Concrete," ASTM International, West Conshohocken, PA, 2003, 3 pp.

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AUTHOR_AFFILIATION

ACI member Kyle A. Riding is a Postdoctoral Researcher at the Swiss Federal Institute of Technology, Lausanne, Switzerland. He received his MS and PhD from the University of Texas at Austin, Austin, TX. He is a member of ACI Committee 201, Durability of Concrete.

ACI member Jonathan L. Poole is an Engineer at Wiss, Janney, Elstner Associates, Inc., Dallas, TX. He received a BS, MS, and PhD from the University of Texas at Austin. He is a member of ACI Committee 207, Mass Concrete, and 305, Hot Weather Concreting.

ACI member Anton K. Schindler is an Associate Professor in the Department of Civil Engineering at Auburn University, Auburn, AL. He received his MSE and PhD in civil engineering from the University of Texas at Austin. He is a member of ACI Committees 211, Proportioning Concrete Mixtures; 231, Properties of Concrete at Early Ages; 237, Self-Consolidating Concrete; and E803, Faculty Network Coordinating Committee.

ACI member Maria C. G. Juenger is an Assistant Professor of civil, architectural, and environmental engineering at the University of Texas at Austin. She received her PhD in materials science and engineering from Northwestern University, Evanston, IL. She is a member of ACI Committees 201, Durability of Concrete; 231, Properties of Concrete at Early Ages; 236, Material Science of Concrete; and E802, Teaching Methods and Educational Materials.

Kevin J. Folliard, FACI, is an Associate Professor in the Department of Civil, Architectural, and Environmental Engineering at the University of Texas at Austin. He received his PhD in civil engineering from the University of California at Berkeley, Berkeley, CA, in 1995. He is a member of ACI Committee 201, Durability of Concrete; 318, Concrete Building Code; and the ACI Publications Committee. He received the ACI Young Member Award for Professional Achievement in 2002.