![]() ·Table of Contents ·Civil Engineering | Damage Level Evaluation and Characterisation by Acoustic Emission and Acousto-Ultrasonics in Concrete Under Compressive LoadsApostolos Tsimogiannis, Athanassios AnastassopoulosENVIROCOUSTICS S.A. El. Venizelou 7 & Delfon, 11452 Athens, Greece E-mail: envac@otenet.gr Barbara Georgali HELLENIC CEMENT RESEARCH CENTER LTD. 15 K. Pateli Str., 14123 Athens, Greece Contact |
| ID | Age (days) | A/C | W/C |
| A | 2 | 4 | 0.60 |
| A | 7 | 4 | 0.60 |
| A | 28 | 4 | 0.60 |
| B | 2 | 3 | 0.50 |
| B | 7 | 3 | 0.50 |
| C | 2 | 3 | 0.65 |
| C | 7 | 3 | 0.65 |
| Table 1: Specimen specifications and data. | |||
The equipment used were a PAC MISTRAS-2001 AE system and a PAC C-101-HV pulser. The sensors used for pulsing and receiving were PAC R6, 60kHz resonant with PAC 1220A preamplifiers. The sensors used were chosen for their high sensitivity, frequency response for concrete measurements[6] and their ability to be used for ultrasonic velocity measurements according to ASNT recommendations[2].
Microscopy results are available for specimens A for all three ages. Prior to the test each specimen was loaded to 150kN to remove AE produced from debris (dust, small particles etc.) on the surfaces of the specimen and to allow for any irregularities on its surface to settle. All specimens were compressed to failure and monitored throughout simultaneously by AE and AU. During compression one AE sensor was constantly receiving AE signals from the specimen. The AU pulses were generated at specific loads. Synchronous triggering of pulser and AE systems was used. The AE acquisition system recorded both features and waveforms for further analysis.
Fig 1: Microscopy results for specimen A, all ages. |
4.1 AE Data Analysis Philosophy and Pattern Recognition
Fusing data from AE and AU (acquired simultaneously) required separation at the analysis stage. A usual approach in AE analysis is the treatment of data as a whole and the observation of characteristics such as signal signature, cumulative energy and its evolution etc.
Due to the complexity of investigating AE data for all specimens and attempting to correlate with other findings it is difficult for the analysts to draw conclusions and much effort is required. The conclusions presented in section 4.2, although significant, contain only a small fraction of the information contained in the AE data as they rely on overall observations. The application of Pattern Recognition (PR)[9][10] to the data was made in an attempt to overcome such problems and limitations. The method is numerical so care must be taken for the preparation of the data. Due to the large dynamic range in some of the AE features a non-linear axis conversion was performed based on logarithmic functions. Subsequently the data were normalized so as to achieve a non-dimensional space. Envirocoustics SA pattern recognition software (Noesis)[7] was used for all PR and data manipulation. The Max-Min Distance[7][9] algorithm was applied to the data for the discrimination of signal groups and the set-up of a starting point for the analysis. Based on the results a k-NNC[7][10] supervised PR algorithm was trained to an accuracy greater than 97.8%. This algorithm was then applied to all sets. Typical results are shown in Figure 4a and 4b. The success of the algorithm to distinguish the AU pulser and receiver signals from other data. At its final form the algorithm had 100% success in recognizing pulser signals. Having such a means to separate the data the progress of different types of signals, which may signify different signal source, can be monitored and more detailed conclusions can be made. The following sections describe the results from these procedures.
4.2 Overall AE Activity
The data collected during compressive loading to fracture of the specimens provided information regarding the initiation and evolution of changes in the material and resulting damage.
The results were such, so as to provide indications about differences in the manner in which the specimens fracture and possibly the mechanisms that cause damage depending both on age and composition of the specimens. This is observed in Figures 2 and 3 were various overall activity data are presented. Figure 2 presents a comparison between specimens of the same composition for three ages (2, 7 and 28 days) for overall AE activity (number of events).
Fig 2: Total number of AE signals for all specimen ages. |
Fig 3: Total number of signals for all specimens age 2 days.
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As can be seen the changes in the overall behavior are distinct as are the slopes of the curves with younger specimens giving off more emission at lower loads. The 7 day specimens for all compositions gave less emission than any other age (see Figure 2b) and the 2 day specimens produced more medium energy emission at lower loads which diminished as the load was increased (see Figure 2a and 3a,b,c). Specimens at the age of 28 days had a distinct behavior with relatively little emission until the fracture load was approached. The overall activity, though, was not significantly higher than the 2 day specimens. Because the 2 and 28 day specimens have very different mechanical properties it can be said that the emission, to be more or less equal, has to come from different sources (mechanisms).
If the AE results are compared to the microscopy findings it can be observed that the lower emission at 7 days may be due to factors such as the small reduction in overall air void content. The overall activity seems to depend on the A/C ratio (see Figure 3), whereas the effect of the W/C ratio appears to be small. Figure 3 presents a comparison of the three compositions used at the same age (2 days). It is evident that specimens B and C (A/C=3) produce more AE at intermediate loads which reduces as the fracture load is approached, than specimen A (A/C=4). The changes introduced by variations in the W/C ratio have more of a qualitative effect. It is obvious, though, that the amount of information is such that it renders the task of correlating AE to microscopy difficult through classical AE analysis.
4.3 PR Class Analysis
PR analysis has provided the mentioned discrimination in AE signal classes (denoted C1-C6, Figures 4a,b) and AU signals (denoted Pulser, Receiver, Figures 4a,b). A brief description of conclusions made through the investigation of microscopy, AE and AU measurements for some of the classes is presented in Table 2.
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| Fig 4: Typical PR results. a) Energy vs Time, b) Signal Strength vs Absolute Energy. | |
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| Fig 5: a) Percent signals per class vs age, b) Percent energy per class vs age. | |
Fig 6: Signal Energy Curve for AU signals and energy per class for AE signals.
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Fig 7: Ultrasonic velocity diagram for all ages |
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