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Cyclic behavior of GFRP strengthened infilled RC frames with low and normal strength concrete

  • Mehmet Emin Arslan EMAIL logo , Ahmet Durmuş and Metin Hüsem
Published/Copyright: August 8, 2018
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Science and Engineering of Composite Materials
From the journal Science and Engineering of Composite Materials Volume 26 Issue 1

Abstract

This paper presents the experimental behavior of plane, non-strengthened and glass fiber reinforced polymer (GFRP) strengthened infilled reinforced concrete (RC) frames with low strength concrete (LSC) and normal strength concrete (NSC) under lateral reversed cyclic loading. For this purpose, eight full-scale, one-bay, one-storey plane and infilled (brick and aerated concrete blocks which are commonly used in RC construction) RC frames with LSC and NSC were produced and in-plane lateral loading tests were carried out. Test results indicate that infill walls considerably change the behavior of frames by increasing rigidity and load carrying capacity. By contrast, GFRP fabric used for strengthening of infilled RC frames improves ductility, load carrying and energy dissipation capacity of infilled frames with LSC and NSC as well. After all the test results were evaluated together, a GFRP strengthened brick infilled frame demonstrated the best performance under cyclic lateral loading.

Keywords: aerated concrete; brick; cyclic loading; GFRP strengthening; RC infilled frame

1 Introduction

As is well known, while structural analysis of frame system structures under lateral loads is performed, the contribution and/or effects of infill walls are neglected. However, the recent earthquakes, and experimental and theoretical studies have depicted that infill walls substantially affect the behavior of reinforced concrete (RC) buildings with a frame system under lateral loads. Indeed, infill walls change stiffness, ductility, damping ratio, period, failure mode and load carrying capacity of the frame system RC buildings [1].

Especially in developing countries in the world, a large part of the existing buildings has been designed in accordance with former standards and often consists of insufficient materials and section properties. As a result, many existing buildings have deficient lateral load resistance, insufficient energy dissipation and can rapidly lose their strength during earthquakes, leading to collapse [2]. The retrofit of seismically deficient structures is one of the solutions to enhance ductility, load carrying and energy dissipation capacity. Recently, the use of fiber reinforced polymer (FRP) composite materials has been proposed as an alternative solution for strengthening of seismically deficient buildings [3], [4]. FRP materials have advantages over other traditional strengthening techniques (cement and epoxy injection steel or RC coating and external prestressing) such as high strength to weight ratio, high resistance to corrosion, excellent durability, and ease and speed of in-place application [5].

Numerous tests have been carried out by researchers to examine the behavior of structural members strengthened by using FRP sheets. In these studies, researchers investigated the effect of the type, amount, and pattern of FRP [6], [7], [8], [9], [10], [11], [12], [13], [14], [15], [16]. Owing to these test results, specifications [17], [18] and numerical models have been developed to estimate the seismic behavior of deficient and strengthened RC buildings [2]. However, most of these studies have been fulfilled using carbon fiber reinforced polymer (CFRP) sheets.

When the technical literature is surveyed, few studies are encountered about the effects of glass fiber reinforced polymer (GFRP) sheets on structural members [19], [20], [21], [22], [23], [24]. Thus, the effects of GFRP sheets on the behavior of infilled RC frames are undetermined. Under the circumstances, the main objective of the current study is to comparatively investigate the behavior of plane and full-scale infilled RC frames with low strength concrete (LSC) and normal strength concrete (NSC), strengthened by using GFRP under lateral reversed cyclic loading. The reason for choosing LSC for comparison is to reflect the behavior of existing seismically deficient buildings. At the end of the study, drift ratio, lateral load carrying and energy dissipation capacity, stiffness degradation and displacement ductility of the RC frame were determined and suggestions are made.

2 Materials and methods

As it was already mentioned, the experimental behavior of plane and strengthened infilled RC frames under lateral reversed cyclic loading was investigated. For this purpose, eight full-scale, one-bay, one-storey, plane frames, RC frames infilled with brick and aerated concrete blocks were produced using LSC and NSC. Thereafter, GFRP strengthening was applied to one of each series of infilled RC frames. Labeling of strengthened and non-strengthened RC frames is given in Table 1.

Table 1:

Labeling of reinforced concrete (RC) frame test specimens.

LabelingDescription of the specimens
PRCF-1Plane RC frame with LSC
PRCF-2Plane RC frame with NSC
RCF-1Brick infilled RC frame with LSC
RCF-2Brick infilled RC frame with LSC and strengthened using GFRP
RCF-3Brick infilled RC with using NSC
RCF-4Brick infilled RC frame with NSC and strengthened using GFRP
RCF-5Aerated concrete blocks infilled RC frame with NSC
RCF-6Aerated concrete blocks infilled RC frame with NSC and strengthened using GFRP

  1. GFRP, glass fiber reinforced polymer; LSC, low strength concrete; NSC, normal strength concrete; RC, reinforced concrete.

2.1 Materials

Mixture proportions of NSC and LSC used for producing the frames are given in Table 2. CEM II/B-M (P-LL) 32.5-R cement was used and the dosage was kept constant at 370 kg/m3 with 0.5 W/C ratios and 225 kg/m3 with 0.9 W/C ratios for NSC and LSC, respectively. Characteristic compressive strength of NSCs and LSCs was determined as 25.14 MPa and 9.75 MPa and elasticity modulus of the concretes was determined as 28,670 MPa and 11,245 MPa, respectively.

Table 2:

Mixture proportions of normal strength concrete (NSC) and low strength concrete (LSC).

Mixture proportionsAggregates (kg/m3)Saturation water (kg/m3)Mixing water (kg/m3)Cement

(kg/m3)
Sieve size (mm)
0.5–1.01.0–2.02.0–4.04.0–8.08.0–16.0
NSC265.50265.50265.50442.50531.007.080185370
LSC265.35265.35265.35442.25530.407.076225250

Producing infill walls was fulfilled using 13.5×19×19 cm horizontal coring bricks and 60× 25×19 cm aerated concrete blocks. Some mechanical and physical properties of horizontal coring bricks and aerated concrete blocks are given in Table 3 .

Table 3:

Some mechanical and physical properties of brick and aerated concrete blocks.

Infill wall materialDimensions (cm)Average compressive strength (MPa)Modulus of elasticity (MPa)Unit weight (kg/m3)
Horizontal coring brick13.5×19×195.22000600
Aerated concrete block60×25×193.31095500
Table 4:

Some mechanical properties of steel rebars used in the test specimens.

Rebar diameter (mm)Average yield strength (MPa)Average tensile strength (MPa)Average rupture strength (MPa)Yield strain (%)Rapture strain (%)
85105704900.2323
124805554650.2322
144705504550.2222

2.2 Details of test specimens and strengthening technique

Dimensions and reinforcement details of the test frames are given in Figure 1. Reinforcement of the test specimens is detailed in accordance with the Turkish Seismic Code [25]. Dimensions of frame and foundation are given in cm. Also, rebar diameters are shown in mm. Some mechanical properties of steel rebars are given in the Table 4. The reinforcement ratio of the beam is 0.005 and 0.015 for columns. Dimensions of the columns and beams are 250 mm×250 mm. In addition, 50 mm and 100 mm stirrup spacings were used for the confinement zone and mid zone, respectively. These stirrup spacing values are 75 mm and 150 mm for beam elements. Figure 2 also illustrates the process of infill wall and concrete plaster applications.

Figure 1: Dimensions and reinforcement details of the test frames.
Figure 1:

Dimensions and reinforcement details of the test frames.

Figure 2: Application of infill wall and concrete plaster.
Figure 2:

Application of infill wall and concrete plaster.

GFRP sheets have been used for the strengthening of the infilled RC frames. Some physical and mechanical properties of the GFRP sheets are given in Table 5. Synthetic resin based adhesive with 1 g/ml unit weight was used to apply the GFRP sheets. The application steps of GFRP sheets to the infilled RC frames are given in Figure 3. As seen in the figures, firstly, adhesive was wiped on as a thin layer. After that, a thicker layer of adhesive was applied as a thin layer and the GFRP sheet was placed on the infill wall.

Table 5:

Some physical and mechanical properties of glass fiber reinforced polymer sheet.

Tensile strength (MPa)Modulus of elasticity (MPa)Unit weight of area (g/m2)Thickness (mm)
220070,0005100.5
Figure 3: Application steps of glass fiber reinforced polymer sheet to the infilled reinforced concrete (RC) frames.
Figure 3:

Application steps of glass fiber reinforced polymer sheet to the infilled reinforced concrete (RC) frames.

2.3 Test setup, instrumentation and loading history

Test setup, loading system and instrumentation are given in Figure 4. The foundations of test specimens were anchored to the strong floor by assembly bars. A servo-hydraulic actuator was used to apply reversed cyclic lateral loads to the top of the test frames. The applied loading protocol used in the study is given in Figure 5. Lateral loads and top displacements were measured by means of a load cell with 500 kN load measurement capacity and 200 mm linear potentiometric displacement transducer, respectively. These values were recorded by a data acquisition system to the computer.

Figure 4: Test set-up of reinforced concrete (RC) frames.
Figure 4:

Test set-up of reinforced concrete (RC) frames.

Figure 5: Loading protocol used in the test.
Figure 5:

Loading protocol used in the test.

3 Results

3.1 Hysteretic responses of test specimens

General views of test frames under lateral reversed cyclic loading and the hysteretic load-displacement curves of test frames at the end of the test are given in Figures 6 and 7 , respectively.

Figure 6: General views of test frames under lateral reversed cyclic loading. (A) PRCF-1, (B) PRCF-2, (C) RCF-1, (D) RCF-2, (E) RCF-3, (F) RCF-4, (G) RCF-5, (H) RCF-6.
Figure 6:

General views of test frames under lateral reversed cyclic loading. (A) PRCF-1, (B) PRCF-2, (C) RCF-1, (D) RCF-2, (E) RCF-3, (F) RCF-4, (G) RCF-5, (H) RCF-6.

Figure 7: Hysteretic load-displacement curve of test frames.
Figure 7:

Hysteretic load-displacement curve of test frames.

PRCF-1: The hysteretic load-displacement curve of a plane RC frame produced using LSC coded as PRCF-1 is given in Figure 7A. As seen from the figure, the behavior of PRCF-1 is practically symmetrical for pull and push directions. Maximum loads obtained from cyclic loading and corresponding displacements for push and pull are 47.76 kN–48.51 mm and 45.08 kN–49.78 mm, respectively. PRCF-1 reached maximum load carrying capacity at 2.28% drift ratio. PRCF-1 carried 37 kN load at 3.5% drift ratio as well.

PRCF-2: Then behavior of a plane RC frame produced using NSC coded as PRCF-2 is similarly symmetrical for pull and push directions like PRCF-1 (Figure 7B). Maximum loads and displacements for push and pull directions of PRFC-2 are 77.61 kN–44.72 mm and 71.01 kN–52.38 mm, respectively. PRCF-2 reached maximum load carrying capacity at 2.10% drift ratio. PRCF-2 carried 60 kN load at 3.5% drift ratio as well.

RCF-1: The hysteretic load-displacement curve of a brick infilled RC frame produced using LSC coded as RCF-1 is given in Figure 7C. It is clearly seen from the figure that the behavior of the test frame is almost symmetrical for both directions. Load carrying capacities and corresponding displacements of RCF-1 for push and pull directions are 214.92 kN–13.08 mm and 196.39 kN–12.78 mm, respectively. In addition, RCF-1 reached its maximum load carrying capacity at 0.6% drift ratio. When loading was kept on, a rapid decrease at load carrying capacity was observed at 1.93% drift ratio (115.95 kN). RCF-1 carried 52 kN load at 3.5% drift ratio as well.

RCF-2: The hysteretic response of a brick infilled RC frame produced using LSC and strengthened with a GFRP sheet coded as RCF-2 is given in Figure 7D. The load-displacement curve of RCF-2 is also symmetrical for pull and push directions. Maximum loads and displacement for push and pull directions of RCF-2 are 331.32 kN–25.04 mm and 306.52 kN–24.72 mm, respectively. The load decrease of RCF-2 after maximum load is more gradual with respect to RCF-1. RCF-2 reached load carrying capacity at 1.18% drift ratio and at 3.5% drift ratio, the frame carried 160 kN lateral load.

RCF-3: The hysteretic load-displacement curve of a brick infilled RC frame produced using NSC is given in Figure 7E. The maximum load and displacement obtained from the test for push and pull directions are 289.15 kN–13.26 mm and 288.13 kN–15.16 mm, respectively. The test frame reached its maximum load at 0.71% drift ratio. When loading was kept on, the load carrying capacity suddenly decreased at 1.35% drift ratio (231.314). Also, RCF-3 carried 61 kN load at 3.5% drift ratio as well.

RCF-4: The hysteretic load-displacement curve of a brick infilled RC frame produced using NSC and strengthened using a GFRP sheet is given in Figure 7F. The maximum load and displacement obtained from the test for push and pull directions are 410.71 kN–26.77 mm and 381.71 kN–26.43 mm, respectively. The test frame reached its maximum load at 1.26% drift ratio. The load decrease after the maximum load is gradual as in the RCF-2 test frame. In addition, RCF-4 carried an approximately 175 kN lateral load at 3.5% drift ratio.

RCF-5:Figure 7G shows that the hysteretic load-displacement curve of infilled with aerated concrete block RC frame produced using NSC coded as RCF-5 is almost symmetrical. The maximum load and displacement obtained from the test for push and pull directions are 148.91 kN–28.08 mm and 135.74 kN–24.13 mm, respectively. The test frame reached its maximum load at 1.14% drift ratio. The load decrease after the maximum load is more gradual than those of RCF-1 and RCF-3 test frames. In addition, RCF-5 carried an approximately 100 kN lateral load at 3.5% drift ratio.

RCF-6: The hysteretic load-displacement curve of infilled with an aerated concrete block RC frame produced using NSC and strengthened using GFRP sheets is given in Figure 7H. The maximum loads and displacement obtained from the test for push and pull directions are 177.22 kN–31.89 mm and 165.00 kN–32.94 mm, respectively. The test frame reached its maximum load at 1.50% drift ratio. RCF-6 had the most gradual load decrease after maximum load and carried approximately 130 kN lateral load at 3.5% drift ratio.

4 Discussion

Test results of plane and GFRP strengthened infilled RC frames with LSC and NSC under lateral reversed cyclic loading have been discussed in terms of load carrying capacity, energy dissipation capacity, displacement ductility and stiffness degradation.

4.1 Load carrying capacity

Load-displacement envelope curves of test frames are illustrated in Figure 8. As seen in the figure, infill walls and the GFRP sheets used for the strengthening of test frames considerably increased the load carrying capacity of plane frames. The load carrying capacity increased most for the RCF-4 test frame. This was followed by the RCF-2 test frame. This result shows that infill material significantly affects the RC frame behavior. Although, brick infilled RCF-3, when aerated concrete block infilled RCF-5 and RCF-6 frames were produced using NSC, their load carrying capacities were lower than that of the RCF-2 test frame. A bar graph is given in Figure 9 to see more clearly the load carrying capacities of the test frames.

Figure 8: Load-displacement envelope curves of test frames.
Figure 8:

Load-displacement envelope curves of test frames.

Figure 9: Load carrying capacities of the test frames.
Figure 9:

Load carrying capacities of the test frames.

It was observed during the test that GFRP sheets worked tension diagonally under reversed cyclic loading. By contrast, GFRP undertook an important responsibility by preventing brittle failure.

4.2 Displacement ductility

The displacement ductility is the ratio of the maximum deformation that a structure or element can undergo without a significant loss of initial yielding resistance to the initial yield deformation. However, it was not easy to determine yield points for the specimens directly from the lateral load-displacement curves. For each specimen, the load-displacement envelope curve was used to define the yield and maximum displacements according to the criteria for equivalent elastoplastic energy absorption used by Park [26] as seen in Figure 10. The ultimate displacement Δu corresponded to a 15% drop of the peak load. The displacement ductility was calculated from the ratio of ultimate displacement to yield displacement Δu/Δy [26], [27], [28]. Displacements at yield, maximum and ultimate loads and displacement ductility of test specimens are shown in Table 6 and Figure 11.

Figure 10: Determination of yield and ultimate displacements according to criteria for equivalent elastoplastic energy absorption.
Figure 10:

Determination of yield and ultimate displacements according to criteria for equivalent elastoplastic energy absorption.

Table 6:

Displacements at yield and ultimate loads and displacement ductility of the test frames.

Test framesLoading directionsFy (kN)Fmax (kN)Fu (kN)Δy (mm)Δmax (mm)Δu (mm)Δu/Δy
PRCF-1Push (+)45.7547.7940.6238.0248.5169.091.82
Pull (−)42.2145.0838.3137.0549.7867.281.81
PRCF-2Push (+)70.0277.6165.9734.0644.7273.212.15
Pull (−)60.1571.0160.3630.1452.3871.212.36
RCF-1Push (+)162.77214.93182.693.7913.0822.735.99
Pull (−)161.85196.39166.933.8212.7823.556.16
RCF-2Push (+)208.61306.52260.545.6024.7242.177.53
Pull (−)211.17331.32281.625.5125.0441.707.56
RCF-3Push (+)218.07289.15238.134.0116.5421.265.30
Pull (−)214.30288.13244.914.0915.1622.905.60
RCF-4Push (+)260.25381.71324.455.4026.4340.207.44
Pull (−)279.60410.71349.105.4326.7640.167.40
RCF-5Push (+)123.18148.94126.573.3528.0835.2610.53
Pull (−)105.90135.74115.383.8124.1335.739.38
RCF-6Push (+)138.51177.22150.644.1631.8964.5815.52
Pull (−)132.91164.97140.225.0132.9472.4514.46
Figure 11: Displacement ductility of the test frames for pull and push directions.
Figure 11:

Displacement ductility of the test frames for pull and push directions.

When the displacement ductility values under cyclic loading were analyzed, the highest ductility was obtained for RCF-5 and RCF-6 which had lower load carrying capacity than those of brick infilled RC frames.

4.3 Energy dissipation capacity

Total dissipated energy was calculated by cumulatively collecting the areas underneath the load-displacement curve for each cycle. The cumulative energy dissipation capacities of the test frames at a particular drift ratio are shown in Figure 12.

Figure 12: Cumulatively dissipated energy of the test frames.
Figure 12:

Cumulatively dissipated energy of the test frames.

As seen in Figure 12, the dissipated energy was small in the elastic stage. When the test frames reached the elastoplastic stage, the amount of the dissipated energy of the test frames increased with increasing damage. After reaching the peak load, the load-carrying capacity of the test frames began to decrease gradually, but the energy-dissipation capacity still slowly increased. As seen in the figure, infill walls increased the energy dissipation capacity of the plane frames. The highest energy was dissipated for the RCF-4 test frame and this was followed by the RCF-2 test frame. These results reveal the importance of GFRP sheets and the material used for producing infill walls with regard to frame behavior. The dissipated energies of the RC test frames at 3.5% drift ratio are given in Figure 13.

Figure 13: Cumulatively dissipated energy at 3.5% drift ratio level.
Figure 13:

Cumulatively dissipated energy at 3.5% drift ratio level.

4.4 Stiffness degradation

Stiffness degradation is a parameter used to evaluate the overall response of specimens. In order to assess stiffness degradation, the secant stiffness was computed for each loading cycle at a particular drift level. The secant stiffness was calculated using a straight line between the maximum load and corresponding displacement points for the positive and negative directions in a load cycle. Stiffness degradation-drift ratio curves of the test frames are given in Figure 14. It is clearly seen from the curves that stiffness of the RC test frames continuously decrease with increasing drift ratio, as cumulative damage in the frames increases throughout the test. In addition, each frame experienced severe stiffness degradation at the end of the test. By contrast, initial stiffness of the test frames is given in Figure 15. As seen in the figure, the highest initial stiffness occurred in the RCF-4 test frame.

Figure 14: Stiffness degradation of the test frames.
Figure 14:

Stiffness degradation of the test frames.

Figure 15: Initial stiffness of the test frames.
Figure 15:

Initial stiffness of the test frames.

4.5 Failure patterns of the test frames

The failure pattern of infilled frames under cyclic loading can differ by span/height ratio. In this study, brick infilled RCF-1 and RCF-3 test frames lost their load carrying capacities by crushing of infill walls, cover and core concrete around beam-column and column-base joints. Even if diagonal cracks occurred for the aerated concrete infilled RCF-5 test frame, the infill wall did not overturn out of the plane direction of the frame. Brick infill walls were crushed under reverse cyclic loading, but none of the brick remained dispersed around owing to the GFRP sheet for RCF-2 and RCF-4 test frames. The crack pattern of RCF-6 is similar to the RCF-5 test frame. By contrast, crack amount increased for the test frames strengthening with GFRP and accordingly, crack widths decreased, whereas, damage to the plane and non-strengthened RC frames centered on the lower end of the column, and cracks distributed uniformly throughout the columns. Failure patterns of the test frames are seen in Figure 16.

Figure 16: Failure patterns of the test frames. (A) PRCF-1, (B) PRCF-2, (C) RCF-1, (D) RCF-2, (E) RCF-3, (F) RCF-4, (G) RCF-5, (H) RCF-6.
Figure 16:

Failure patterns of the test frames. (A) PRCF-1, (B) PRCF-2, (C) RCF-1, (D) RCF-2, (E) RCF-3, (F) RCF-4, (G) RCF-5, (H) RCF-6.

5 Conclusions

This paper presents the experimental behavior of plane and GFRP strengthened infilled RC frames with LSC and NSC under lateral reversed cyclic loading. For this purpose, eight full-scale, one-bay, one-storey plane and infilled (brick and aerated concrete blocks) RC frames with LSC and NSC were produced and loaded laterally. Based on the test results of this study, the following conclusions can be made:

  1. GFRP sheets used for strengthening of infilled RC frames with LSC and NSC under lateral reversed cyclic loading considerably increased load carrying capacity, energy dissipation capacity and displacement ductility. In addition, GFRP sheets prevented dispersal around the remains of the infill wall. These results indicate that GFRP sheets used for strengthening contribute to preventing loss of life and properties.

  2. When the initial stiffness, load carrying and energy dissipation capacities of the RC frames are all evaluated together, the RCF-4 infilled frame has the best performance such that load carrying capacity, energy dissipation capacity and initial stiffness value of the RCF-4 frame are higher than those of other test frames 24%–760%, 28%–1165% and 1.356 times, respectively.

  3. Load carrying capacities of brick infilled RC frame produced using LSC coded as RCF-1 and brick infilled RC frame produced using LSC and strengthened with GFPR sheets coded as RCF-2 are approximately 21%–122% higher than RC frames infilled with aerated concrete block produced using NSC (RCF-5) and strengthened with GFPR (RCF-6). This result shows that choosing infill material is very important to obtain a higher load carrying capacity.

  4. The highest displacement ductility is obtained for the RCF-6 frame. This result shows that infill walls with aerated concrete blocks contribute to the ductility of the RC frames.

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Received: 2017-02-15
Accepted: 2018-03-26
Published Online: 2018-08-08
Published in Print: 2019-01-28

©2019 Walter de Gruyter GmbH, Berlin/Boston

This work is licensed under the Creative Commons Attribution 4.0 Public License.

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  14. The influence of the WC-Co composite microstructure model on stress field heterogeneity at the microstructure level: FEM based study
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  25. UV sensing optode for composite materials environment monitoring
  26. On crushing characteristics of hybrid sandwich aluminum-cardboard panels reinforced with glass fiber composite rods
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  28. A research on the preparation of oil-adsorbing hydrophobic porous resins by high internal phase emulsions (HIPEs) template
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  43. Microstructures, interface structure and room temperature tensile properties of magnesium materials reinforced by high content submicron SiCp
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  47. Thermal conductivity of unidirectional composites consisting of randomly dispersed glass fibers and temperature-dependent polyethylene matrix
  48. Effects of Waste Eggshells addition on Microstructures, Mechanical and Tribological Properties of Green Metal Matrix Composite
  49. Investigation of porosity effect on flexural analysis of doubly curved FGM conoids
  50. Review Article
  51. Utilization of tailings in cement and concrete: A review
  52. Research Article
  53. Equivalent stiffness prediction and global buckling analysis using refined analytical model of composite laminated box beam
  54. Mechanochemical synthesis of zincite doped with cadmium in various amounts
  55. Size-dependent vibration analysis of graphene-PMMA lamina based on non-classical continuum theory
  56. Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells
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  59. The low-velocity impact and compression after impact (CAI) behavior of foam core sandwich panels with shape memory alloy hybrid face-sheets
  60. Effect of granulometric distribution on electromagnetic shielding effectiveness for polymeric composite based on natural graphite
  61. The enhancement of filament winding in marine launching rubber gasbag
  62. Research on ELID Grinding Mechanism and Process Parameter Optimization of Aluminum-Based Diamond Composites for Electronic Packaging
https://doi.org/10.1515/secm-2017-0060
Keywords for this article
aerated concrete; brick; cyclic loading; GFRP strengthening; RC infilled frame
Creative Commons
BY 4.0

Articles in the same Issue

  1. Analysis on the impact response of fiber-reinforced composite laminates: an emphasis on the FEM simulation
  2. Artificial neural network for predicting the flexural bond strength of FRP bars in concrete
  3. Cyclic behavior of GFRP strengthened infilled RC frames with low and normal strength concrete
  4. Durability of basalt fiber-reinforced polymer bars in wet-dry cycles alkali-salt corrosion
  5. Effect of B4C particle size on the mechanical properties of B4C reinforced aluminum matrix layered composite
  6. Enhanced dielectric properties of BaTiO3 ceramics with cerium doping, manganese doping and Ce-Mn co-doping
  7. Free and forced vibration analysis of rectangular/circular/annular plates made of carbon fiber-carbon nanotube-polymer hybrid composites
  8. Influence of nano-SiO2 on the bonding strength and wear resistance properties of polyurethane coating
  9. Investigation of wear behavior of nanoalumina and marble dust-reinforced dental composites
  10. Negative effect of clay fillers on the polyvinyl alcohol biodegradation: technical note
  11. Photocatalytic activity of Cu2O/ZnO nanocomposite for the decomposition of methyl orange under visible light irradiation
  12. Sub-surface mechanical properties and sub-surface creep behavior of wood-plastic composites reinforced by organoclay
  13. Surface integrity in wire-EDM tangential turning of in situ hybrid metal matrix composite A359/B4C/Al2O3
  14. The influence of the WC-Co composite microstructure model on stress field heterogeneity at the microstructure level: FEM based study
  15. Vibration-damping characterization of the basalt/epoxy composite laminates containing graphene nanopellets
  16. A review on nanocomposite hydrogels and their biomedical applications
  17. Optimization and simulation analysis of structure parameters of OPCM ultrasonic longitudinal wave actuating element
  18. Research Article
  19. Preparation of POSS-triol/wollastonite composite particles by Liquid phase mechanochemical method and its application in UV curable coatings
  20. Research on preload relaxation for composite pre-tightened tooth connections
  21. Dough moulding compound reinforced silicone rubber insulating composites using polymerized styrene butadiene rubber as a compatibilizer
  22. Hydration And Microstructure Of Astm Type I Cement Paste
  23. Effects of NiO content on the microstructure and mechanical properties of AgSnO2NiO composites
  24. Overall buckling behaviour of laminated CFRP tubes with off-axis ply orientation in axial compression
  25. UV sensing optode for composite materials environment monitoring
  26. On crushing characteristics of hybrid sandwich aluminum-cardboard panels reinforced with glass fiber composite rods
  27. Preparation and characterization of Ni-Cu composite nanoparticles for conductive paints
  28. A research on the preparation of oil-adsorbing hydrophobic porous resins by high internal phase emulsions (HIPEs) template
  29. Material characteristics of random glass-mat-reinforced thermoplastic under cryogenic thermal cycles
  30. Differentiation of non-black fillers in rubber composites using linear discriminant analysis of principal components
  31. Research Article
  32. Efficiency of TiO2 catalyst supported by modified waste fly ash during photodegradation of RR45 dye
  33. Synthesis and performance of polyurethane/silicon oxide nano-composite coatings
  34. Study on preparation of magnesium-rich composite coating and performance enhancement by graft modification of epoxy resin
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  36. Mechanical and wear properties of polyetheretherketone composites filled with basalt fibres
  37. Mechanical Properties of Al 25 wt.% Cu Functionally Graded Material
  38. Research Article
  39. Weight reduction of a carbon fibre composite wheel
  40. Synthesis, electrical properties, and kinetic thermal analysis of polyaniline/ polyvinyl alcohol - magnetite nanocomposites film
  41. Seismic Behaviour of TRC-Strengthened RC Columns under Different Constraint Conditions
  42. Characterization of neat and modified asphalt binders and mixtures in relation to permanent deformation
  43. Microstructures, interface structure and room temperature tensile properties of magnesium materials reinforced by high content submicron SiCp
  44. Research Article
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  46. Mechanical and tribological properties of B-C-N coatings sliding against different wood balls
  47. Thermal conductivity of unidirectional composites consisting of randomly dispersed glass fibers and temperature-dependent polyethylene matrix
  48. Effects of Waste Eggshells addition on Microstructures, Mechanical and Tribological Properties of Green Metal Matrix Composite
  49. Investigation of porosity effect on flexural analysis of doubly curved FGM conoids
  50. Review Article
  51. Utilization of tailings in cement and concrete: A review
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  53. Equivalent stiffness prediction and global buckling analysis using refined analytical model of composite laminated box beam
  54. Mechanochemical synthesis of zincite doped with cadmium in various amounts
  55. Size-dependent vibration analysis of graphene-PMMA lamina based on non-classical continuum theory
  56. Automated, Quality Assured and High Volume Oriented Production of Fiber Metal Laminates (FML) for the Next Generation of Passenger Aircraft Fuselage Shells
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  58. An investigation of the stitching effect on single lap shear joints in laminated composites
  59. The low-velocity impact and compression after impact (CAI) behavior of foam core sandwich panels with shape memory alloy hybrid face-sheets
  60. Effect of granulometric distribution on electromagnetic shielding effectiveness for polymeric composite based on natural graphite
  61. The enhancement of filament winding in marine launching rubber gasbag
  62. Research on ELID Grinding Mechanism and Process Parameter Optimization of Aluminum-Based Diamond Composites for Electronic Packaging
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