A method, a system, and non-transitory computer readable medium for aging analysis are provided. The method includes performing stress simulations for a plurality of process, voltage, temperature (PVT) conditions for a circuit, the circuit including one or more devices, extrapolating device level stresses obtained from the stress simulations into device level parameter degradations to a desired circuit age; and performing degradation simulations for the circuit for the same PVT conditions based on the device level parameter degradations. Each degradation simulation for a PVT condition of the plurality of PVT conditions is performed using the device level parameter degradations associated with the same PVT condition.

Methods, systems, and apparatus, including medium-encoded computer program products, for computer aided design of physical structures using generative design processes. A method includes obtaining one or more load cases and one or more design criteria for a modeled object, the one or more design criteria comprising a build material strength model indicating strength relationships between thickness of an object feature and build angle for that object feature resulting from additive manufacturing; iteratively modifying a three dimensional shape of the modeled object in accordance with the one or more design criteria and the one or more load cases, including applying the strength relationships between the thickness of the object feature and the build angle for that object feature on a per-element basis during numerical simulation of the modeled object; and providing the three dimensional shape of the modeled object for use in manufacturing a physical structure.

A method can comprise: performing a finite element static analysis of an inspected blade of an inspected bladed rotor, the inspected blade having a repair blend profile modeled thereon, the repair blend profile exceeding a threshold repair size; performing a finite element modal analysis of the inspected blade having the repair blend profile; performing a fatigue assessment based on results from the finite element static analysis and the finite element modal analysis, the fatigue assessment including limits based on material properties of the inspected blade, the material properties based on test results at a threshold significance level; and repairing the inspected bladed rotor with the repair blend profile in response to the fatigue assessment meeting a deterministic criteria.

The present disclosure provides advantageous probabilistic models and applications for component (e.g., titanium component) design optimization, and related methods of use. More particularly, the present disclosure provides advantageous probabilistic models, systems and applications for component design optimization and related methods of use, and where the probabilistic models, systems and applications can accurately predict the life/failure of components (e.g., titanium components) based on material microstructure statistics and/or product mission specifics and/or variations. Disclosed are probabilistic systems and methods for predicting dwell fatigue behavior of a component (e.g., titanium component). The present disclosure advantageously provides an analytical modeling framework that captures the various physics-based mechanisms for dwell fatigue damage accumulation, crack nucleation, crack propagation and fracture in components or materials (e.g., anisotropic components/materials). The probabilistic modeling framework thereby enables the prediction of dwell fatigue behavior as a function of microstructure (e.g., material microstructure statistics) and/or loading conditions (e.g., product mission specifics).

A method of predicting low-cycle fatigue crack initiation and propagation behaviors under a multi-scale framework includes the following steps: S1, providing a calculation method for low-cycle fatigue crack initiation and propagation damages under a multi-scale framework; S2, determining a slip system where a maximum damage is located and an accumulated damage of all slip systems by calculation using the calculation method in S1; S3, a crack initiating and propagating in a direction towards the slip system where the maximum damage is located when the accumulated damage reaches a critical value; and S4, conducting calculation repeatedly until a predicted crack length reaches a fracture length of a low-cycle fatigue specimen under test conditions.

A method for modeling joints using User Element (UEL) techniques by analytically eliminating a series of internal degrees of freedom for representing actual weld or joint stiffness in structures. The resulting formulation is in closed-forms enabling computational accuracy and simplicity for structural applications. For spot joint, the detailed ring type of finite elements required to achieve a reasonable accuracy can be replaced by a simple finite element mesh using just four user elements. The UEL joint modeling method offers accurate stress calculation results by comparing with the mesh-insensitive structural stress method coupled with a detailed explicit joint representation of joints. The UEL method can also be applied for modeling seam welded joints, e.g., MIG, laser, and friction stir welds. The explicit representation of weld fillet geometry required by existing methods is no longer needed by the UEL plate/shell elements without losing any accuracy.

A programmable integrated circuit includes configuration circuitry configured to receive configurations of a user design for the programmable integrated circuit. Each of the configurations implements the user design using at least some unique circuitry in the programmable integrated circuit relative to the other ones of the configurations. The configuration circuitry is further configured to implement the user design in a first one of the configurations. The configuration circuitry is further configured to move the user design from the first one of the configurations to a second one of the configurations to cause effects of aging processes in circuits in the programmable integrated circuit that are not aged by the first one of the configurations.

A method of optimising one or more physical properties of an alloy comprises conducting a plurality of trials per an experimental design on a plurality of candidate alloys. Each trial comprises measuring a plurality of values of each physical property of the candidate alloys for different values of a plurality of parameters, wherein the parameters comprise respective concentrations of the two or more constituents, and one or more process parameters. The method further comprises fitting the plurality of values of the physical property and the plurality of parameters to a response surface model; and determining, from the fitted response surface model, optimised values of the parameters that optimise the respective responses; wherein the response surface model describes a non-linear relationship between a time integral of each of the physical property and a linear combination of non-linear functions of the plurality of parameters.

A system and method for performing circuit design analysis obtains a circuit design comprising cells. The cells are associated with cell types. Aging parameters of a core analytical model are determined for each of the cell types in the circuit design to generate a calibrated analytical model. Aging effects for the cells are determined based on the calibrated analytical model and target stress conditions. An aged timing model is determined for the cell types based on the aging effects, an unaged timing model, and the target stress conditions.

The disclosure discloses a multi-time-scale reliability evaluation method of a wind power IGBT considering fatigue damage and a system thereof. Lifetime information of a power device is comprehensively extracted by using multiple time scales. An electro-thermal coupling model of an IGBT module is established to obtain a junction temperature data. A steady-state junction temperature database of the IGBT in different aging states is established. Based on a SCADA monitoring data, the junction temperature data is outputted in real-time through the electro-thermal coupling model and a real-time thermal stress cycle number is calculated in a short-term time-scale profile, and a wind speed probability distribution curve is obtained in a long-term time-scale profile. A maximum thermal stress cycle number that the IGBT can withstand in different aging stages is obtained in advance and a cumulative damage degree and an estimated lifetime of the IGBT of the wind power converter are calculated.