ISSN: 2643-6736
Abdolrasoul Ranjbaran^{1}*, Mohammad Ranjbaran^{2} and Fatema Ranjbaran^{3}
Received: February 08, 2020 Published: February 15, 2020
Corresponding author: Abdolrasoul Ranjbaran,Department of Civil and Environmental Engineering, Shiraz University, Shiraz, Iran
DOI: 10.32474/ARME.2021.03.000153
Failure analysis diagram (FAD) is an important tool in safety assessment of cracked structural systems. Conventional methods for determination of (FAD) is expensive and contain epistemic uncertainty. Toward the remedy, failure is considered as change of state of the system. Based on logical reasoning and concise mathematics a method, called the change of state philosophy is developed and used for analysis of change, and is shown to be a unified tool for development of (FAD). The work is verified via concise logical reasoning and comparison of the results with those of the others.
Keywords: Failure Analysis Diagram;Logical Failure Analysis;Persian Curve;State Functions;Phenomenon Functions
A conventional tool for assessing the integrity of structures containing cracks is, fracture mechanics and the failure assessment diagram (FAD) [1-18]. The (FAD) is a combination of the limiting conditions for load, the crack size and fracture toughness or yielding stress. The abscissa is the load ratio and the ordinate is the toughness ratio. The toughness ratio is defined as a function of the load ratio. Classical fracture mechanics contains epistemic uncertainty and is unreliable. As a result, the conventional (FAD) is also unreliable. Change of state philosophy (CSP), which is digested in the Persian curve (PC) is developed as a remedy for removal of uncertainty as follows.
The failure phenomenon is conceived as a change in the state of the system [19-39]. A decreasing parameter (capacity, toughness and etc.) of the system is called stiffness. The inverse of stiffness is called flexibility. The (CSP) formulation is commenced by the obvious Eq. (1) as shown in Figure1, in which (k_{SS}=k_{S}-k_{C}) is the system stiffness at changed state, (k_{S}) is the system stiffness at intact state, (k_{C}) is the change stiffness, (f_{SS}=f_{S}+f_{C}) is the system flexibility at the change state, (f_{S}) is the system flexibility at change state and (f_{C}) is the change flexibility.
Equation (1) is rearranged to obtain the (k_{SS}) and (k_{C}), in Eq. (2):
In which the phenomenon functions (collection of the failure function (FR) and the survive function (SR)) are defined in Eq. (3):
Since obvious concepts are used, then the proposed method is free of epistemic uncertainty. The unknown parameters (k_{C}&f_{C}) should be explicitly determined. The investigation for explicit definition of the aforementioned functions, is continued in the next paragraph via definition and construction of the so called, state functions.Consider (k_{s} = f_{s}= 1) and insert into Eq. (3) to define the destination function (D) and the origin function (O), which are collectively called the state functions and the state ratio (R) in Eq. (4).
The state functions may be considered as solution of the boundary value problems in Eq. (5), in which (min) and (max) denote minimum and maximum respectively:
The (R) with one end in the infinity, is not a good working parameter. Therefore, the state variable (ξ ∈[0,1]) with a zero value (ξ = 0) at the origin and a unit value (ξ =1) at the destination is defined. The state variable is the phenomenon’s abstract lifetime. In terms of the state variable, the boundary value problems in Eq. (5) are rewritten in Eq. (6):
The authors used their experience in structural mechanics, finite element method, mathematics and extensive research [37] to solve Eq. (6). The results is the state functions defined in Eq. (7):
Via definition of the (k_{SS}) and the (f_{SS}) and the concept of crack compliance (f_{C}) in fracture mechanics [4], the authors detected a fact that, the (f_{C}) is directly proportional to the (k_{S})! This detection is called “the Persian Principle of Change (PPC)”. In view of this principle the (f_{C}) is defined in Eq. (8):
Insertion of Eq. (8) into Eq. (3) concluded in the general definition for the phenomenon functions in Eq. (9):
Toward better definition and preparation for using reliable data, Eq. (9) is rewritten in Eq. (10) in terms of the positive control parameters (aM) and (b) [37].
To this end the proposed formulation is mathematically in abstract form. Consequently, it is a certain universal formulation, in a sense that it is independent of geometry, coordinates, material properties, size and changing agent. Therefore, it equally applies to all natural-phenomena.
The proposed formulation is derived based on logical reasoning and concise mathematics, consequently, it is reliable and free of epistemic uncertainty. To prepare for determination of control parameters for a phenomenon, the (F_{R}) is renamed as Persian-Fasacurve (P_{F}), the (S_{R}) is renamed as Persian-Shiraz-curve (PS) and the two collectively called the Persian curve (P_{C}), defined in Eq. (11), in which (P_{O}) is the ordinate of the origin point (O) and (P_{T}) is the ordinate of the truncated (end) point (T).
In comply with the vocabulary of human knowledge, the (PS) is the unified equation for capacity and reliability representing a decreasing data and the (P_{F}) is the unified equation for the probability and fragility representing an increasing data. Moreover, in comply with the common practice in stochastic analysis the (probability) density distribution, here called the Persian-Zahedancurve (P_{Z}), and defined as the derivative of phenomenon functions with respect to the ( ξ ) and is casted in Eq. (12), in which (D(1)) is derivatives of (D) with respect to ( ξ ).
In order to determine the control parameters, Eq. (11) is rearranged as in Eq. (13):
Eq. (13), in terms of control parameters (a_{M}& b) is nonlinear. An artifice is used, to determine the control parameters (a_{M}& b) from Eq. (14) in terms of the (KPS) ordinates, equally applies, to both of increasing and decreasing data as shown in Figure 2.
The Key Points (KPS) are defined as the Origin point (O), the Middle point (M), the end point (T) and the Next point (N) (a point between the other three), in Eq. (15) and shown in Figure 2 for both of decreasing and increasing data:
Intensive investigation of the reliable capacity data in the literature [37], concluded into the key points, on the lower bound of capacity, in Eq. (16).
O(0.0,1.0) N (0.25, 0.86) M (0.5, 0.4) T (1.0, 0.1) (16)
Insertion of Eq. (16) into Eq. (14) concluded into the control parameters, in Eq. (17).
Substitution of control parameters in Eq. (17) into Eq. (11) and Eq. (12) concluded in the unified capacity function (PSU), unified fragility function (PFU) and unified density function (PZU), in Eq. (18).
Persian curve is defined in terms of an abstract life time called state variable in a unit interval (ξ ∈[0,1]) . In real phenomena, the lifetime (λ ) is selected in a truncated interval ( [ , ]) o T λ ∈ λ λ , where ( O λ ) is the lifetime origin and ( T λ ) is the lifetime destination. Lifetime is a characteristic of the system. In common practice the ratio (to make it user friendly) of a predefined parameter (FY) and an intentionally defined one (FE) is expressed as lifetime (λ ), as in Eq. (19).
For the case of structural systems (FY) is the yield stress, (FE) is the Euler’s stress and lifetime (λ ) is the relative slenderness ratio, as in Eq. (20). The other parameters are (Le) effective length, (r) is radius of gyration, (E) is initial modulus.
For systems containing flaw the lifetime (λ ) is denoted by (Lr). In order to use the Persian Curve, the lifetime (λ ) should be mapped on the state variable (ξ ), as in Eq. (21).
Example 2: Compare the Unified Persian curve with the FAD defined in Eq. (23).
Solution: The FAD from Eq. (23) (KIII) [6, 9, 12, 18] is compared with the unified Persian curve (PSU) in Figure 4. The lifetime is mapped onto the state variable as ( 2.25 ) r L = ξ . A set of test data (TEST) [40] is also shown. The (KIII) goes through the unified key points, but the test results located under it, that is contain uncertainty and is not reliable. In order to show the power of the work in fitting curve on data, the function in Eq. (24) (KIIIR) is also shown in Figure 4.
These figures shown that although all of the conventional (FAD)s go through some of the key points, but overestimate the test results, then contain epistemic uncertainty. The validity of the (PC) as logical (FAD) is verified.
The conventional (FAD) is based on conventional fracture mechanics, which is based on singularity of stress at crack tip. Stress singularity at crack tip is a wrong concept, then the conventional fracture mechanics and the (FAD) contain epistemic uncertainty and are not logical. On the other hand, the proposed formulation is logical and reliable. The parameter (Lr) is defined as the ratio of the applied stress over the yield stress. Experience in determination of ultimate strength of structures shown that the combination of the material and geometric properties, in the form of the relative slenderness ratio (λ ), as in Eq. (20), is the necessary and sufficient condition. Note that, Eq. (20) is the inverse of the current definition of (Lr) when applied stress is selected as the Euler’s stress. Consequently, replacement of the (Lr) with the (λ ) is recommended. The (PC) used as (FAD) is necessary and sufficient for failure analysis of structures with cracks.
The following conclusion obtained from this study. The failure phenomenon is conceived as the change of state of the system. Based on logical reasoning and concise mathematics, the change of state is expressed in terms of the Persian curve. The Persian curve is completely calibrated from four key points on real world data. Making use of reliable data in the literature, the unified control parameters and the unified Persian curves are explicitly expressed in term of the state variable. The unified Persian-Shiraz curve (PSU) is proposed as a reliable (FAD). Validity of the (FAD) is verified via concise mathematical logics, and comparison of the results with those of the others. It is shown that the (PC) is sufficient for failure analysis of structures containing cracks.
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