Y.-D. Song's research while affiliated with Nanjing University of Aeronautics & Astronautics and other places
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Publications (59)
Fatigue crack growth (FCG) mechanisms of Ni-based superalloy FGH4098 at 650℃-800℃ was investigated. The increased temperature and prolonged dwell time enhance the FCG rate by 2-3 orders of magnitude due to grain boundary (GB) oxidation. Characterization at the propagating crack tips with EBSD, TKD, TEM and EDX shows deformation (e.g. dislocations a...
Short fatigue crack propagation (SFCP) behaviour of a powder metallurgy (PM) superalloy (i.e. FGH4098) for aeroengine turbine disc application was investigated at room temperature and 650 °C in vacuum (10⁻³ pa) by in-situ fatigue test. The SFCP mechanism was analyzed by the microstructural characterization and assessment of the SFCP rate. The resul...
The macro and mesoscale deformation and damage of the PM nickel-based superalloy FGH4098 under low cycle fatigue loading at elevated temperatures were investigated using both SEM/EBSD characterization and crystal plasticity finite element (CPFE) simulations. The results indicate that higher temperature leads to more severe macroscale damage i.e. la...
In this study, the effects of microstructure, temperature and dwell time in a loading cycle on low cycle fatigue (LCF) and stress relaxation behaviours of a powder metallurgy Ni-based superalloy (i.e. FGH4098) for aeroengine turbine disc application were studied along with detailed microscopic characterisation of fracture features and deformation s...
In this study, GH4169 alloy was hot-corroded using NaCl+Na2SO4 salts; the microstructures, composition and hardness of hot corrosion (HC) layer were investigated, and fatigue tests were conducted on the as-received and hot-corroded GH4169 alloy. The results show that HC causes oxidation and sulfidation in GH4169 alloy. The formed sulfide layer is b...
The prediction of the stress distribution plays a key role when replacing conventional metallic components with ceramic matrix composites (CMCs) ones in the turbine engine. Furthermore, the complete thermal-mechanical properties of a CMCs component cannot be obtained through experimentation. Accordingly, a numerical method to calculate the thermal-...
A numerical simulation analysis of mechanical chip morphology and residual stress for Ti6Al4V alloy was conducted under different cutting speed and feed rate. Johnson-Cook constitutive model and shear failure model were selected in the simulation procedure. The correlations between the mechanical chip morphology and surface residual stress were det...
Powder metallurgy (PM) Ni-based superalloys are widely used for aeroengine turbine disc applications due to their excellent mechanical properties and good corrosion resistance at elevated temperatures. Understanding the fatigue crack growth (FCG) mechanisms of PM Ni-based superalloys is important for both disc alloy development and life prediction...
Machined surface condition of nickel-based superalloys has an important influence on the functional performance of the components. Proper selection of cutting parameters could improve surface finish and increase service life of parts and components. This research work bases on an experimental and statistical study of turning GH4169 nickel-based sup...
Foreign object damage (FOD) is a common accident that happens in aeroengines, especially in fan and compressor blades. Accurate prediction of the fatigue strength of the fan/compressor blade materials following FOD is important for the repair and maintenance of aeroengines. This paper was based on the experiment part of Ref. [13], and fatigue stren...
Effects of thermal exposure (TE) on high cycle fatigue (HCF) behaviours in Ni-based superalloy GH4169 have been investigated in this study. GH4169 specimens were thermally exposed at 650 °C for 1, 2, 7, 14 and 21 days before fatigue test. These TEs produced eruptions, bulge-like features and pits at surface due to oxidation of carbides/nitrides. Fa...
p>The role of oxygen in enhanced fatigue cracking in an advanced Ni-based superalloy for turbine disc application has been evaluated in fatigue crack initiation and propagation stages along with static oxidation tests. It is found that the grain boundary oxide intrusion has a layered structure. The microstructure- and deformation-dependent grain bo...
A new multiaxial fatigue life prediction model has been proposed in this paper. The concepts of nonlinear continuum damage mechanics and critical plane criteria were incorporated in the proposed model. The shear strain-based damage control parameter was chosen to account for multiaxial fatigue damage under constant amplitude loading. Fatigue tests...
Fatigue tests under variable amplitude multiaxial loading were conducted on notched specimens of titanium alloy TC4. The key issues of fatigue life estimation under variable amplitude multiaxial loading for notched components have been researched. Multiaxial fatigue critical area of notched specimen was determined first. Then, fatigue damage contro...
Multistage fatigue tests were conducted on the single-edge-notch tension specimens of Ni-based superalloy GH4169. Fatigue crack growth data at different stages were recorded with the surface replica technique. Continuum damage mechanics incorporating critical distance theory was used to evaluate fatigue crack initiation life. Then, small and long f...
Fatigue tests under multiaxial loading were conducted on Ni-based superalloy GH4169 tubular specimens. The microstructures of fracture surfaces under different loading paths were compared. Several multiaxial fatigue criteria were reviewed and evaluated with multiaxial fatigue test data. The criteria of equivalent strain, maximum shear strain and Ka...
The methodology of probabilistic fatigue life prediction for notched components based on smooth specimens is presented. Weakestlink theory incorporating Walker strain model has been utilized in this approach. The effects of stress ratio and stress gradient have been considered. Weibull distribution and median rank estimator are used to describe fat...
The tension-compression fatigue behavior for needled C/SiC composite at room temperature was studied and compared with the properties under tension-tension fatigue loading. The results show that the tension-compression fatigue strength of the needled C/SiC composites is slightly lower than that under tension-tension loading. Hysteresis phenomenon c...
An anisotropic damage constitutive model for needled ceramic matrix composites was proposed based on continuum damage mechanics. The effects of both tensile damage and shear damage were considered in the model. The stress-strain curves of the material were obtained by tensile and shear tests and the parameters of the constitutive model obtained by...
An approach for calculating stress intensity factors was proposed based on the first several items of the theoretical polynomial solution of the elastic crack tip stress field in infinite body, and the stress intensity factors were calculated by fitting the finite element solution of elastic crack tip stress field in actual crack bodies. This metho...
Both the proportional and nonproportional multiaxial fatigue tests were conducted on two kinds of notched specimens of titanium alloy TC4. The multiaxial fatigue critical area of notched specimen is considered as the location experiencing the maximum damage. It is unsatisfactory to predict the multiaxial fatigue life with the local stress and strai...
Surface replication method was utilized to monitor the small fatigue crack initiation and growth process of single-edge-notch tension specimens fabricated by nickel base superalloy GH4169. Three different stress levels were selected. Results showed that small fatigue cracks of nickel base superalloy GH4169 initiated from grain boundaries or surface...
General weight functions of the corner quarter-elliptical crack in three-dimensional rectangular plate were studied. Uniform, higher-precision and relatively wider-application-range approximate expressions of reference stress intensity factors were obtained, by using the reference finite element data of the stress intensity factor when the crack su...
Based on the air-gun impact test device, the foreign object damage (FOD) simulation test of TC4 titanium alloy plate specimens was conducted at different impact angles. The high cycle fatigue (HCF) strength of smooth and impact damage samples was obtained with the step-test method. The relationship among the impact angles, impact positions, macrosc...
The tensile behavior of cross-ply C/SiC ceramic-matrix composites (CMCs) at room temperature has been investigated. Under tensile loading, the damage evolution process was observed with an optical microscope. A micromechanical approach was developed to predict the tensile stress–strain curve, which considers the damage mechanisms of transverse mult...
An estimation method for the fatigue life of notched specimen under multi-axial loading is proposed. The multi-axial fatigue damage parameter in every part of notched specimen is calculated based on a critical plane criteria. The location of notched specimen with the maximum damage parameter is taken as a multi-axial fatigue dangerous point. The cr...
Fatigue tests under variable amplitude multiaxial loading were conducted on titanium alloy TC4 tubular specimens. A method to estimate the fatigue life under variable amplitude multiaxial loading has been proposed. Multiaxial fatigue parameter based on Wu–Hu–Song approach and rainflow cycle counting and Miner–Palmgren rule were applied in this meth...
A computing method on equivalent thermal conductivity of plain braided C/SiC composites material was proposed based on finite element method. Mesoscopic structure of materials was studied firstly, including microscopic model of carbon fiber bundles with matrix and single-cell model. Effects of porosity on the matrix equivalent thermal conductivity...
An estimation method for fatigue life under multi-axial random loading was proposed. Firstly the rain-flow counting method was used to identify shear strain cycles on each plane. The shear strain cycles were taken as a main control parameter of multi-axial fatigue damage. Then the maximum normal stress and normal strain range within each shear stra...
The uniaxial tensile behavior of unidirectional C/SiC ceramic-matrix composites at room temperature has been investigated. An approach to predicting the uniaxial tensile stress–strain curve of the unidirectional ceramicmatrix composites is developed. The Budiansky–Hutchinson–Evans shear lag model is used to describe the microstress field of damaged...
Based on the traditional structural optimization method, a structural/material optimization method for turbine frame was developed in consideration of the effects of structural parameters and properties of materials on the performance of turbine frame. The original optimization problem was decomposed into structure level and the material level. The...
Based upon the microphotographs of the needled ceramic matrix composites(CMCs), appropriate representative volume elements(RVE) were selected to establish a single-cell model for predicting the elastic properties of needled ceramic matrix composites. The effect of porosities on the elastic properties of matrix and fiber bundles was considered, and...
The matrix random cracking of ceramic matrix composite was simulated by Montel Carlo model. The shear-lag model was used to analyze the micro-stress field of the damaged composites, and the formula of the stress-strain behavior was derived. The uniaxial tensile experiment of unidirectional-C/SiC composites at ambient temperature has been performed,...
Low cycle fatigue (LCF) life prediction and critical distance analysis for TC4 alloy notched specimens were conducted. The correlation between the critical distance and fatigue life, load ratio, stress concentration factor and their influence on the fatigue life prediction were studied. The result suggests that the critical distance of TC4 alloy is...
A kind of unit cell for 2.5 dimension C/SiC composites was established by extracting the boundary of warp, fitting the curve using robust least square and simplifying the fitted curve. The elastic properties of 2.5 dimension C/SiC composites were predicted using dual-scale model; the dual-scale model was micro-scale which considered the scale of ma...
A novel constitutive model was developed for composite by combining the theory of macro and micro scale coupled constitutive model and the virtual displacement principle. The displacement within the subcell was expanded in terms of the global strains and the fluctuating displacements. Then the virtual displacement principle was used to construct th...
Based on the stress distribution in the bonded and de-bonded region of ceramic matrix composite (CMC) with matrix cracks, the sliding mechanism of CMC was investigated, and the analytical method for estimating damping capacity in unidirectional CMC was derived. Numerical examples show that: (1) CMCs' inherent damping capacity is very small. The dam...
A study on uniaxial tensile strength of the unidirectional ceramic matrix composites was presented in this paper using micromechanical approach. The shear lag model was used to obtain the micro stress field of the damaged composites. The statistical matrix cracking model and fracture mechanics interface debonding criterion were used to determine ma...
The higher-order theory was developed to three-dimension, coefficients of temperature function were replaced by surface-averaged temperature to be primary variables of equations, and the concept of sub-cells was canceled. The number of equations was reduced so that computational efficiency was increased effectively. During the thermal analysis of r...
A generalized method of cell (GMC) with weak interface was developed to model the interface debonding within continuum fiber reinforced composite. To accomplish this work, the average displacement continuum condition between sub-cells in original GMC was modified by employing weak interface theory. Then the average strain of subcell was expressed i...
The influence of fiber Poisson contraction on matrix cracking development of ceramic matrix composites under unidirectional tensile was studied in this paper. The micro stress field was analyzed by combining the Coulomb's friction law and the Lame formulation. The matrix cracking development was determined by the critical matrix strain energy crite...
The stress-strain response of cross-ply fiber-reinforced ceramic composites laminates under quasi-static loading was discussed by using a micromechanical approach. The cross-ply modified shear lag model was used to analyze the micro stress field of the damage composites. The critical matrix strain energy criterion and the Nair de-bond criterion wer...
The failure problems of porous ceramic materials were analyzed using the lattice model and statistical methods. Finite element model of porous ceramic materials was established firstly. Then, the failure process of porous ceramic materials was simulated by using self-adapt load technique. Finally, the simulation results were analyzed statistically....
A multi-scale constitute model for ceramic matrix composite (CMCs) was presented in this paper by using high-fidelity generalized method of cell (HFGMC). Based on the microstructure and damage characteristics of CMCs, a representation volume element (RVE) and damage variables were defined. Then, the evolution of damage variables was calculated by H...
The micromechanical finite element method and the nonlinear spring element for the interface were employed to predict the effective behavior of MMCs. The results indicate that weak interfacial bonding reduces the macro mechanical properties of MMCs. A weak interfacial bonding reduces the elastic modulus of MMCs. The Constant Compliant Interface (CC...
The interaction between a round inclusion and a crack under thermal and remote mechanical loading is analyzed based on the body force method (BFM). The traction-free condition on the crack line is mended so that the couple effect of thermal and remote mechanical loading could be taken into account and the accuracy could be improved. The traction-fr...
Based on Monte-Carlo method, uniform simulation and Gaussian simulation were used to simulate the stochastic fiber location. The digital images of the material cross-section were generated by the simulation method. Grids were generated by meshing the digital image pixels. Based on these grids the GMC (generalized method of cell) is used to calculat...
The efficient reformulation of higher-order theory was deduced. Averaged quantities at the interface were the primary variables, and the averaged quantities were used to replace the coefficient of temperature. By using the heat exchange equations, the relationship between heat flux and average temperature was established, and temperature field was...
This paper analyzed the penalty function pseudo-nodes displacement consistent method. Based on these methods, non-pseudo-nodes displacement consistent method is presented, which solved the problem of the displacement consistency between meshes with different densities. The formulations of the methods are deduced. Consequently the contradiction betw...
The unified macro and micro mechanics constitutive model was used to investigate the influence of microstructural geometry, such as fiber shape and fiber packing array, on the composite initial yielding surfaces under multi-axial loading. Under longitudinal stress, composites reinforced by fibers with square cross section have the same yielding str...
Based on the Bodner-Partom (B-P) visco-elastic-plastic constitutive theory, after developing a self-adaptive time integration method for the constitutive equation, a user defined subroutine was developed and implemented into the general purpose nonlinear finite element software ANSYS. The software takes material deformation, cyclic and variable loa...
The relation between macroscopic characteristic and microscopic characteristic is studied. Microscopic characteristic is imposed on a point in macroscopic composite object. A micromechanics model is presented based on the hypothesis of the periodicity in the composite microstructure. In the model, the microscopic deformation fields are described wi...
According to the principle of equal damage of flight mission spectrum and corresponding composite spectrum to an engine due to fatigue, creep and thermal impact, compounding 5 flight mission profiles and a functional check profile, composite route flight mission profiles are obtained. Rotating speed spectrum are calculated from altitude-velocity ch...
Citations
... Hu et al. [9] suggested that the low cycle fatigue (LCF) properties of FGH96 superalloy were sensitive to surface defects, such as surface scratches and surface inclusion. Jiang et al. [11,12] discussed the mechanism of fatigue crack growth controlled by microstructural features in the review, indicating that the appliance of X-ray computed tomography, diffraction contrast tomography, and in situ fatigue testing could provide a better and more intuitive assessment of fatigue crack growth behavior. The microstructure and defects of the matrix of PM greatly affect low-cycle fatigue; however, surface integrity is also critical since fatigue cracks are initiated on the surface [13]. ...
... As a result, the aerospace industry desperately needs alloy materials that can withstand high temperatures [2]. Powder superalloys are well suited for such critical components [3][4][5] and fourth-generation powder superalloy turbine disks are in development to withstand temperatures reaching 815 • C. As temperature and performance requirements rise, new design concepts, compositions and processes must be developed for a new generation of powder superalloy turbine disks [6][7][8] and to mitigate the length and high cost of new material development. High entropy alloys (HEAs) with novel designs are an increasing focus of research, and related concepts are gaining in popularity. ...
... Globally, the tool manufacturers applied ultra-hard thin film coating to provide better cutting performances like low friction coefficient and thermal conductivity, higher resistance to abrasive wear, prevent destructive high temperature effects in cutting zone and chemical inertness. The most commonly used monolayer coated carbide tools with several deposition material films include TiC, 11,12 TiN, [13][14][15][16] TiCN, 17,18 TiAlN, [19][20][21][22] TiAlxN, 23 AlTiN, [24][25][26][27] specifically applied to machining of hardened steels that replaces costly ceramic and CBN tools. In the present research, as the hardness of workpiece of 57 HRC, there might be the chances of more catastrophic failure for ceramic tools compared to coated carbides because of its high brittleness and low toughness. ...
... Such oxidation processes can promote enhanced crack initiation processes and multiple crack formation along the grain boundaries, which can give rise to crack coalescence events and therefore enhanced crack propagation rate. This is also linked to a greater extent of intergranular fracture features and results in reduced lifetime [16,17]. ...
... The damage phase-field acts to degrade the elastic energy of the material, resulting in a degradation of the stiffness matrix and a rearrangement of the internal stress field (Molnár and Gravouil, 2017). The phase field method differs from other continuum damage mechanics (CDM) approaches (Wu et al., 2018;Dapaah et al., 2020) in that the phase field method avoids damage broadening through the length scale parameter ( ) (de Borst and Verhoosel, 2016), provides an estimate of a displacement discontinuity, and utilizes an energetic formulation to allow for different types of crack evolution, rather than requiring various criteria to model damage initiation, branching, or propagation (Steinke et al., 2017). The usefulness of the phase-field method in studying damage behavior in hard biological tissues was recently demonstrated by Maghami et al. (2021a,b), particularly due to its ability to accurately predict complex damage behavior involving crack branching and multiple damage fronts. ...
... When the angle was large, the inhibitory effect was intense and could even make the crack propagation stop. This is consistent with the conclusion reached by Zhu [11] and Wu [15] when studying the fatigue crack growth behavior of nickel-based alloy GH4169. ...
... Based on the above analysis, many studies are conducted in-depth on the failure rate of materials, but the most only focuses on constant cyclic loading. In fact, many components operate under random and complex loads [22,23], so the uncertainty of the load should be considered during the modeling process of failure rate. In this paper, the mapping relationship between external cyclic stress and fatigue life is studied, and the conversion mechanism between the probability distribution of cyclic stress and the probability distribution of Ti-6246 alloy fatigue life is revealed. ...
... Two traditional critical plane approaches for multiaxial fatigue analysis presented in this section, and the recent processes on multiaxial notch fatigue analysis are introduced. According to the multiaxial fatigue test results and models established for notched components, fatigue initiation usually starts from a specific plane [85][86][87], in which one or more characteristic parameters play a dominate role. ...
... Notches in real components play a decisive role in the fatigue process. There are numerous approaches to evaluate notched structures, e.g., support factor concepts, respectively, stress gradient-based approaches [7,25], the Theory of Critical Distance (TCD) by Taylor [26], approaches based on the strain energy density [27], energy field intensity approaches [28,29], concepts based on the weakest-link theory [30,31], probabilistic models [32,33], among others. Spaggiari et al. [34] present a comparison between the TCD and the classical stress gradient based approach for the fatigue assessment of notched components and point out the advantages and disadvantages of the approaches. ...
... Thus, validity verification research works have been subsequently performed. Specifically, in their following research, 87 65,66,89,90 initially analysed the fatigue strength of notch components on the basis of a newly defined critical plane-based multiaxial fatigue model. However, they only considered stress-strain data collected from notch tip and overlooked the impact of notch effect, thus the predicted results overall tend to be conservative. ...