# Multilevel Seismic Damage Behavior Correlation Analysis for RC Framed Structures

Authors: Jianguang Yue
Journal: Advances in Materials Science and Engineering
 (2018)

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## Abstract

Five structural levels, that is, material level, section level, member level, storey level, and structure level, were proposed to analyze the multilevel nonlinear mechanism of the reinforced concrete (RC) framed structures. Based on the presented deformation equivalent principle, a generalized stiffness damage model was developed for each structural level. At each structural level, the stiffness damage value can be calculated by the integration of the material stiffness damage. Furthermore, an impact factor was proposed to reflect the damage correlations between different structural levels. In order to verify this method, the proposed method was used to study the damage evolutions at various structural levels of a 12-storey frame structure. The numerical model utilizing the proposed analysis method produces results in good agreement with the test results of the 12-storey frame structure. It shows that the proposed method is useful to assess the structure multilevel damage performance and to design a new structure.


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## Body

## 1. Introduction

In damage mechanics of concrete structures, a damage model can directly calculate the inherent damage states of structures, members, or sections. For this reason, in the performance-based design method (PBDM), the damage degree is often evaluated in an explicit way by introducing the damage performance levels, which corresponds to the seismic intensity levels. The performance levels describe damage with the aid of damage models. However, in actual design works by now, the damage model is usually used to assess the nonlinear behavior for structure level or member level and very limitedly used in designing. The most important reason is that there is no any perfect damage model to describe the damage states for every structural level, and the damage correlations between the different levels are unknown. That is to say, it is not like the force-based design method which can clearly calculate the force relations between the structure level, storey level, member level, section level, and material level. Therefore, it is necessary to propose a new damage model which can calculate damage for every structural level and find a way to reflect the damage correlations between different structural levels.For different analytical purposes, the damage model can be defined by different mechanical indicators, such as stiffness, deformation, energy, and vibration characteristics. For example, the hysteretic energy-based damage model is often used to evaluate the damage for structure level or member level [1, 2]. In some researches, the deformation has been verified as a good damage indicator not only for the bending-failure-type members (RC columns, beams, and walls) but also for the shear-failure-type members [3]. The deformation-characterized interstorey drift ratio or plastic rotation was used to define the damage model by the study of Banon and Veneziano [4] and Wang et al. [5]. The widely-known Park and Ang damage model [6] was defined by both maximum displacement and plastic energy of dissipation. The strains of concrete and rebar were used to establish a procedure of damage determination for member level by Sharifi et al. [7]. Moreover, the bearing capacity of the M-N relationship can be used to evaluate the damage of section level [8], and the variations of the stiffness or intrinsic period can be used to evaluate the damage of structure level [9].In the theory of engineering mechanics, the stiffness means the deformation-resistant capacity, that is, the ratio of force to deformation, for any structural level. Thus, the stiffness could be an ideal damage indicator for the multilevel damage assessment. In fact, the stiffness-based damage index in a well-known concrete plastic-damage model [10] has been widely used for the nonlinear numerical analysis [11, 12]. It was proposed from the strain equivalent principle [13] that the strain of damage material caused by nominal stress is equal to the strain of undamaged material caused by the effective stress. Furthermore, this stiffness-based damage index using the integrating method with the weight coefficient (such as the lengths or important factors of the damage zones) can be used to predict the damage performance of the structure level [14–16].In this paper, a deformation equivalent principle was firstly proposed based on the strain equivalent principle. Secondly, a generalized stiffness-based damage model was presented for every structural level. Its arithmetic expression in an integrating form and the correlation impact factor were used to analyze the multilevel damage mechanism. As an example, a shaking table seismic test of a single-span 12-storey RC framed structure was analyzed by the proposed method.


## 2. Multilevels for RC Framed Structure

Under earthquake seismic motion, the mechanical behavior-like deformation capacity, bearing capacity of material, member, or structure can be characterized at material level, section level, member level, storey level, and structure level. As shown in Figure1, each structural level can be expressed as the analysis object Oi, in which the letter i means the structural level. The values of i are 1, 2, 3, 4, and 5 for the structure level, storey level, member level, section level, and material level, respectively. An example for the multilevel definition is shown in Figure 1. In Figure 1, the subscript i of Oi,k denotes the structural level i and the subscript k is the object number; that is, Oi,k means the object k at level i, and O1 means the object at structure level (the global structure). The superscript “i,k” of Oj,li,k means it is a part of Oi,k; that is, Oj,li,k means the object l at level j as a part of Oi,k. As shown in Figure 1, the global structure is denoted as O1 and storey 2 is denoted as O2,21. In storey 2 (O2,21), the columns 1, 2, 3, and 4 are denoted as O3,12,2, O3,22,2, O3,32,2, and O3,42,2, respectively, and the beams 1, 2, and 3 are denoted as O3,52,2, O3,62,2, and O3,72,2, respectively. In column 1 (O3,12,2), section 1 can be written as O4,13,1. The material point k of section 1 is denoted as O5,k4,1.Figure 1
Illustration of multilevel damage definition.According to the definition, the affiliation framework of the five structural levels is expressed in Figure1. This affiliation framework shows the analysis object for each structural level. It can be used to find which object is important for the structural mechanism. Moreover, the correlations between different levels can be abstractly expressed (Figure 1). It can represent the correlation between any two different structural levels.


## 3. Deformation Equivalent Principle

In general, local damage in RC structures subjected to a severe seismic motion is usually caused by the microcracking and crushing of concrete, yielding of the steel reinforcement, and bond deterioration of the steel-concrete interfaces. The local damage on a cross section can be adequately evaluated by the degradations of the sectional bending stiffness and moment bearing capacity. The overall combination of all local damages leads to the global stiffness and strength deterioration of the structure. Damage models are used to characterize the damage state of the structure after an earthquake seismic motion and can be used to assess the design aims or the postearthquake bearing capacity. According to the principle of strain equivalence, the damage at material level is defined by the concept of effective stress. The effective stressσ′ is the stress applied on an element of undamaged material with the same deformation of a damaged element subjected to the current stress σ.Essentially, the strain equivalence assumption describes the material stress-strain relation by introducing the damage variabled. Considering this principle can be popularized to any structural level, the definition is reasonably deduced as follows: the effective force F′ (Figure 2) applied to an element of undamaged object (material, cross section, member, storey, or structure level) will have same deformation like a damaged element subjected to the current force F (Figure 2).Figure 2
Generalized force-deformation relationship [17].


## 4. Seismic Stiffness Damage Model

Therefore, a generalized force-deformation relation [17], as shown in Figure 2, can be used to describe the behavior at any structural levels. In Figure 2, point A represents the initial damage state and curve 0AB represents the nonlinear behavior caused by material damage.In Figure2, δ is the generalized deformation for every structural level, and δi, δi,e, and δi,u represent the deformation, elastic limit deformation, and ultimate deformation of level i, respectively; F is the generalized force which corresponds to the generalized deformation δ, Fi represents the force for damaged configuration, Fi,e is the elastic limit bearing capacity; Ki,0, Ki, and Ki,eq are the initial stiffness, secant stiffness, and equivalent stiffness, respectively. The equivalent stiffness Ki,eq represents the damage effect on stiffness of the undamaged configuration and is expressed as(1)Ki,eq=δiKi−δi,eKi,0δi−δi,e.Here, the point A in Figure2 is assumed to represent the initial damage state. Therefore, based on the deformation equivalent principle, the generalized damage variable di is(2)di=1−Ki,eqKi,0.Equation (2) is the generalized stiffness damage variable which can reflect the stiffness degradation for every structural level. This model can also be formulated in the material configuration for thermodynamically stable problems with no temperature time variation. Thus, the mathematical form for the free energy is assumed as [18, 19](3)ψ5ε,d5=1−d5ψ50ε=1−d512ρ0εTσ0=1−d512ρ0εTE0ε,d5=1−EeqE0;Eeq=εE−ε0E0ε−ε0,where ψ5 and ψ50 (i = 5 for material level) are the free energy of damaged material and undamaged material, respectively; d5 is the material stiffness damage variable; ε and ε0 are the strain tensor and elastic limit strain tensor of material, respectively; σ0 is the stress tensor of undamaged material; ρ0 is the material density; and E0 is the initial elastic modulus, Eeq is the equivalent modulus, E is the secant stiffness. Specially, if d5=0, then ψ5ε,d5=0 means the strain energy of undamaged material.The potential energyWi,kp of object Oi,k can be obtained by integrating ψ5 with mass through the volume of Oi,k and expressed as(4)Wi,kp=∫Vi,kψ5dm=∫Vi,k1−d5ψ50ρ0dV=1−d5Wi,kp,0,where Wi,kp,0 is the potential energy of undamaged object Oi,k and Wi,kp,0=∫Vi,kψ0ρ0dV. Thus, the stiffness damage di,k of Oi,k can be calculated from (4) and expressed as(5)di,k=1−Wi,kpWi,kp,0=∫Vi,kψ50dV−∫Vi,k1−d5ρ0ψ50dV∫Vi,kρ0ψ50dV=∫Vi,kd5ρ0ψ50dV∫Vi,kρ0ψ50dV≈∑ei,kd5ψ50∑ei,kψ50,where ∑ei,k means the summation for all elements of object Oi,k. Equation (5) shows that the stiffness damage di,k for any structural level i can be calculated by the material damage d5.If the damagedj,l and the free energy ψj,l0 of object Oj,li,k are known, it has the relationships of ∑ej,lψ50=ψj,l0 and ∑mψj,l0=∑ei,kψ50. The damage di,k of object Oi,k (j>i) can be obtained by substituting these two above relationships into (5), and the resulting expression is as follows:(6)di,k=∑mdj,lψj,l0∑mψj,l0,where ∑m means the summation for total parts of Oi,k and m is the part number of Oi,k. Equation (6) shows that the damage di,k can also be obtained by the summation of dj,l with the weighted coefficient ψj,l0.Therefore, an impact factorγi,kj,l is proposed here to calculate the damage effect from Oj,li,k to Oi,k. Based on (6), its expression is(7)γi,kj,l=dj,lψj,l0∑mdj,lψj,l0,where 0≤γi,kj,l≤1, and the higher value of γi,kj,l means higher damage effect from Oj,li,k to Oi,k.


## 5. Test Model and Numerical Simulation

A shaking table test of a 12-storey RC frame model (Figure3) of the State Key Laboratory of Disaster Reduction in Civil Engineering in Tongji University [20] was used to verify the proposed analysis method of the damage correlations of different structural levels. The ABAQUS computer program [21] was used to perform numerical simulation of the test model which was subjected by the earthquake seismic motions. In the finite element model, the material behavior of concrete was described by the concrete plastic-damage model presented by Lubliner et al. [10], which can calculate the compression and tensile damage of concrete. The concrete was modeled by C3D8R elements which are 8-node linear brick elements with reduced integration and hourglass control. The material behavior of the steel reinforcement was described by an elastoplastic model with 1% strain hardening. The steel reinforcements were modeled by the T3D2 elements which are 2-node linear displacement truss elements and embedded in the concrete elements.The 12-storey model frame structure has one single bay in theX- or Y-direction, a total height of 3.6 m and a storey height of 0.3 m. The plan and elevation views of the structure are shown in Figure 3. The compressive strength of concrete is from 5.74 MPa to 8.20 MPa. The cross-sectional size of all columns and beams are 50 × 60 mm and 30 × 60 mm, respectively. Reinforcement layouts are identical in all beams and columns. The yield strength and ultimate strength of rebar number 1 (nominal diameter is 2.11 mm) are 390 MPa and 560 MPa, respectively. The yield strength and ultimate strength of rebar number 2 (nominal diameter is 0.9 mm) are 327 MPa and 397 MPa, respectively. The average elastic modulus of concrete is 7.75 × 103 MPa.Four earthquake seismic motions were used as the test loading input: (1) El-Centro waves, (2) Kobe waves, (3) Shanghai artificial waves, and (4) Shanghai bedrock waves. The range of the input peak acceleration was 0.090–0.904 g. The standard storey and top storey were subjected by additional masses of 19.4 kg and 19.7 kg, respectively. Totally 54 loading cases were calculated and compared with the test results.In loading case number 53, the values of input peak ground acceleration inX-, Y-, and Z-direction were 0.904 g, 0.769 g, and 0.452 g of EI-Centro waves, respectively. In loading case number 53, vertical cracks occurred at the ends of beams from storey 2 to 8. The damages from storey 3 to 8 were most serious, where the maximum width of cracks was about 4 mm and plastic hinges appeared at the ends of beams. There was almost no damage from storey 11 to 12.As shown in Figure4, the calculated acceleration responses of A2, AY2, A7, and AY7 of loading case number 53 were compared with the test results. The acceleration responses of A2 and A7 were along the X-direction, and the responses of AY2 and AY7 were along the Y-direction. The calculated results agreed well with the test results. It shows that the numerical model can depict the nonlinear seismic responses of the test model with well accuracy. The multilevel damage evolutions of the test model can be analyzed based on the numerical responses. In the following, the loading case number 53 was used to be analyzed with the proposed method.Figure 3
Geometrical details of the 12-storey RC frame test model [20]. (a) Elevation and acceleration sensor placement. (b) Structure plan. (c) Beam cross section. (d) Column cross section.
(a)
(b)
(c)
(d)Figure 4
Comparisons of calculated and tests responses [20]. (a) Case 53: A2 acceleration comparison. (b) Case 53: AY2 acceleration comparison. (c) Case 53: A7 acceleration comparison. (d) Case 53: AY7 acceleration comparison.
(a)
(b)
(c)
(d)


## 6. Multilevel Damage Analysis

### 6.1. Structure Level and Storey Level

The structural final damage state of loading cases number 53 is shown in Figure5(a). The abbreviation PEEQT stands for the equivalent plastic tensile strain which reflects the onset of cracks. According to (6), the stiffness damage evolutions can be calculated for each structural level. Thus, the calculated stiffness damage evolutions of the global structure and each storey (from storeys F2 to F12 in Figure 3) are shown in Figure 5(b). The letter F followed by the number 1 to 12, denotes the floor or storey. The damage of storey F1 was close to zero, so it was not shown in Figure 5(b).Figure 5
Damage results for structure level and storey level. (a) Final damage comparisons of calculation and test [20]. (b) Damage evolutions for storey level and structure level.
(a)
(b)In Figure5, the calculated damages from storeys F3 to F8 were the most serious with the maximum damage value of 0.8. The damage evolution curves show that damages at storeys F2 to F8 occurred almost at the same time. The calculated maximum damage of storey F2 was 0.5. The maximum damage value of the global structure was 0.7. Compared with the test damage states (Figure 5(a)), it shows that the calculated results were in good agreement with the test responses. Moreover, Figure 5(b) reflects the damage mechanism at storey level and structure level. The analysis results indicate that the structure level damage was mainly due to the damages of storeys F5 to F7.


### 6.2. Member Level, Section Level, and Material Level

The columns Z1 to Z12 (Z means column) and beams B1 to B12 (B means beam) were analyzed for the member level. In Figure6, if the damage value was close to zero, it will not be shown.Figure 6
Damage evolutions for (a) member level, (b) section level, and (c) material level.
(a)
(b)
(c)As shown in Figure6(a), the onset of damage of columns Z2 and Z8 and beams from L2 to L8 started at the same time, that is, about 0.25 s. The damage evolutions of beams from L3 to L7 developed faster than other members. At storey F2, the damage evolution of column Z2 developed faster than beam L2. At storey F8, the damage evolution of column Z8 developed faster than beam L8.The maximum damage values of columns Z2 and Z8 were 0.6 and 0.8, respectively. The maximum damage values of column Z2 and beams L3 to L7 were about 0.8. The maximum damage value of beam L8 was about 0.65. The maximum damage values of column Z2 and beam L2 were about 0.5.According to Figure6(a), the damages of storeys from F3 to F7 were mainly due to the beams, the damage of storey F8 was mainly due to the columns, and the damage of storey F2 was due to both columns and beams. Based on this analysis, only the sections of columns Z5 to Z7 and beams L5 to L7 were necessary to be analyzed for the section level (Figure 6(b)). In Figure 6(b), the letters c and b mean the sections of column and beam, respectively.Based on the comparison of Figures5 and 6, it can be found that the damage of section level, member level, storey level, and structure level almost began at the same time (about 0.25 s). The maximum damage values of sections c5, c6, and c7 were small (about 0.3) which corresponded to the damage values of columns Z5, Z6, and Z7. The maximum damage values of sections b5, b6, and b7 were large (about 0.9) which corresponded to the damage values of beams L5, L6, and L7. Therefore, it means that the damages from storey F5 to F7 were mainly caused by the bending-type failures of beams.Thus, only the material points mb5 to mb7 of beam sections L5 to L7 were necessary to be analyzed for material level (Figure6(c)). It can be found that the damage of material level began at the same time with the other structural levels. However, the damages of mb5 and mb6 reached to their peak values earlier than mb7. The damage evolutions of material agreed with the responses of beams L5 and L6.


## 6.1. Structure Level and Storey Level

The structural final damage state of loading cases number 53 is shown in Figure5(a). The abbreviation PEEQT stands for the equivalent plastic tensile strain which reflects the onset of cracks. According to (6), the stiffness damage evolutions can be calculated for each structural level. Thus, the calculated stiffness damage evolutions of the global structure and each storey (from storeys F2 to F12 in Figure 3) are shown in Figure 5(b). The letter F followed by the number 1 to 12, denotes the floor or storey. The damage of storey F1 was close to zero, so it was not shown in Figure 5(b).Figure 5
Damage results for structure level and storey level. (a) Final damage comparisons of calculation and test [20]. (b) Damage evolutions for storey level and structure level.
(a)
(b)In Figure5, the calculated damages from storeys F3 to F8 were the most serious with the maximum damage value of 0.8. The damage evolution curves show that damages at storeys F2 to F8 occurred almost at the same time. The calculated maximum damage of storey F2 was 0.5. The maximum damage value of the global structure was 0.7. Compared with the test damage states (Figure 5(a)), it shows that the calculated results were in good agreement with the test responses. Moreover, Figure 5(b) reflects the damage mechanism at storey level and structure level. The analysis results indicate that the structure level damage was mainly due to the damages of storeys F5 to F7.


## 6.2. Member Level, Section Level, and Material Level

The columns Z1 to Z12 (Z means column) and beams B1 to B12 (B means beam) were analyzed for the member level. In Figure6, if the damage value was close to zero, it will not be shown.Figure 6
Damage evolutions for (a) member level, (b) section level, and (c) material level.
(a)
(b)
(c)As shown in Figure6(a), the onset of damage of columns Z2 and Z8 and beams from L2 to L8 started at the same time, that is, about 0.25 s. The damage evolutions of beams from L3 to L7 developed faster than other members. At storey F2, the damage evolution of column Z2 developed faster than beam L2. At storey F8, the damage evolution of column Z8 developed faster than beam L8.The maximum damage values of columns Z2 and Z8 were 0.6 and 0.8, respectively. The maximum damage values of column Z2 and beams L3 to L7 were about 0.8. The maximum damage value of beam L8 was about 0.65. The maximum damage values of column Z2 and beam L2 were about 0.5.According to Figure6(a), the damages of storeys from F3 to F7 were mainly due to the beams, the damage of storey F8 was mainly due to the columns, and the damage of storey F2 was due to both columns and beams. Based on this analysis, only the sections of columns Z5 to Z7 and beams L5 to L7 were necessary to be analyzed for the section level (Figure 6(b)). In Figure 6(b), the letters c and b mean the sections of column and beam, respectively.Based on the comparison of Figures5 and 6, it can be found that the damage of section level, member level, storey level, and structure level almost began at the same time (about 0.25 s). The maximum damage values of sections c5, c6, and c7 were small (about 0.3) which corresponded to the damage values of columns Z5, Z6, and Z7. The maximum damage values of sections b5, b6, and b7 were large (about 0.9) which corresponded to the damage values of beams L5, L6, and L7. Therefore, it means that the damages from storey F5 to F7 were mainly caused by the bending-type failures of beams.Thus, only the material points mb5 to mb7 of beam sections L5 to L7 were necessary to be analyzed for material level (Figure6(c)). It can be found that the damage of material level began at the same time with the other structural levels. However, the damages of mb5 and mb6 reached to their peak values earlier than mb7. The damage evolutions of material agreed with the responses of beams L5 and L6.


## 7. Damage Correlation Analysis

Although the multilevel damage analysis can respect the structural damage mechanism for different structural levels, it still cannot provide quantitative values to describe the correlations between different structural levels. In this section, the damage correlations were analyzed to explore the inherent nonlinear behavior of the structure and to help designing a new structure. As mentioned above in Section4, the presented impact factor γi,kj,l of (7) was used here to reflect the damage correlations quantitatively.Firstly, the damage effect from storey level to structure level was analyzed (Figure 7(a)). It shows that the impact factor curves of sotreys F4, F5, and F6 started to increase at about 0.25 s and quickly reached to the peak values of 0.39, 0.28, and 0.18, respectively, at about 0.5 s. Then, the impact factor curves of F4, F5, and F6 began to decrease and finally reached to the minimum value of 0.11, and meanwhile the structure reached to its maximum value. The impact factor curves of storeys F2, F3, F7, and F8 also started to increase at 0.25 s and reached to the maximum values of 0.19, 0.15, 0.12, and 0.19, respectively, while then began to decrease, and meanwhile the structure reached to the maximum value. It can be seen from the above results that the structure damage was caused by the storeys F4, F5, and F6 in the beginning and then caused by the storeys F2, F3, F7, and F8. Comparatively, the damage effect from storeys F5 and F6 was the most serious for the global structure. Thus, the damage effect from beam L5 and column Z5 to the storey F5 (Figure8) was analyzed in the following (Figure 7(b)).Figure 7
Damage correlations between different levels. (a) Storey level to structure level. (b) Member level to storey level. (c) Section level to member level. (d) Material level to section level.
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(b)
(c)
(d)Figure 8
The analysis objects of member level, section level, and material level.In Figure7(b), the impact factor values of column Z5 were very close to zero. It indicates that column Z5 did not affect storey F5. While the impact factor curve of beam L5 started to increase at 0.25 s and reached to the maximum value of 0.25, and meanwhile, the storey F5 reached to about half of its maximum value. It indicates that the damage of storey F5 was mainly caused by the beams.Furthermore, the damage effect from two cross sections (one is at the beam end and another is at the middle span in Figure8) and one diagonal section (near the beam end in Figure 8) to beam L5 was analyzed as follows (Figure 7(c)).It can be found that the impact factor values of sections b5-2 and b5-3 were close to zero while the maximum value of section b5-1 was 0.66. That means the damage of beam L5 was mainly caused by the cross-sectional damage at its end which was the bending-type failure. Thus, three material fibers (Figure8) were analyzed to reflect the damage effect from material points to the cross section b5-1. Here, each fiber, including three element nodes, was used as the representative for the material level. The impact factor curves of fiber 2 and fiber 3 were very close, and their values were larger than the value of fiber 1. The impact factor maximum values of fiber 2 and fiber 3 were about three times of fiber 1. It indicates that the damage effect of the bottom fibers was more serious than the fibers at the top of the section.Based on the above analysis, the failure of this 12-storey-framed structure model (noted as objectO1) was the plastic hinge failure mode of beams. The seriously damaged storeys were F5, F6, and F7 in which the damage effect from F5 (noted as O2,51) was the most serious. The damage of F5 was mainly due to the damage of beams which was mainly caused by the cross-sectional damage at the ends of the beam.The impact factor values are listed in Table1. It represents qualitatively the damage effect between different structural levels. It shows the damage effect degree of the level i comes from another level j. For example, about 12% damage of the global structure was caused by the storey F5, and about 25% damage of storey F5 was caused by beam L5. Only 3% damage of the global structure was caused by beam L5, and only 1.7% damage of the global structure was caused by the section L5-1. It can be seen that the damage mechanism of the structure can be described very clearly in a quantitative way. Obviously, this analysis method is very helpful to design a new structure.Table 1
Damage correlations between different structural levels at limit state.
Structural level
Structure
Story F5
Beam L5
Section L5-1
Fiber 3
Stiffness damage
0.769
0.896
0.882
0.951
0.951
γ
i
+
1
i
—
0.120
0.249
0.554
0.425
γ
i
1
—
0.120
0.030
0.017
0.007


## 8. Conclusions

In order to explore the multilevel damage mechanism of the RC framed structure, five structural levels (structure level, storey level, member level, section level, and material level) were proposed as the multilevel analysis objects. Based on the generalized deformation equivalent principle, a generalized stiffness damage model is proposed for every structural level. The stiffness damage for each structural level can be calculated by integrating material stiffness damage. Furthermore, an impact factor was proposed to reflect quantitatively the damage correlations between different levels. As an example, a single-span 12-storey RC framed model was analyzed using this method. The results show that the multilevel damage analysis method can evaluate accurately the damage correlations between different levels. It should be very useful for the damage assessment and design of structures.



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*Source: 2364297-2018-05-10.xml*