Expert Systems with Applications, Journal Year: 2024, Volume and Issue: unknown, P. 125455 - 125455
Published: Sept. 1, 2024
Language: Английский
Expert Systems with Applications, Journal Year: 2024, Volume and Issue: unknown, P. 125455 - 125455
Published: Sept. 1, 2024
Language: Английский
Physics of Fluids, Journal Year: 2025, Volume and Issue: 37(1)
Published: Jan. 1, 2025
When calculating the transient flow around a bridge structure, traditional computational fluid dynamics methods are extremely time-consuming, especially for multiparameter optimization analyses. Inspired by development of deep graph neural networks with mesh this paper describes spatiotemporal prediction framework rapid reconstruction and flows on large-scale unstructured grids. To ensure stability reliability during self-supervised training, causal self-attention mechanism is employed in temporal model. The trained tested dataset containing 40 000 snapshots fields Reynolds numbers ranging from 104 to 105. relative mean square error model predicting velocity pressure found be order 10−3 does not exceed 10%. This demonstrates that capable reconstructing high-dimensional field information low-dimensional data. Furthermore, proposed achieves speedup two orders magnitude compared respect inference. validate its ability infer aerodynamic characteristics, used predict surface pressure, coefficients, streamlines, vorticity. results demonstrate has reliable accuracy, representation, identifying multiscale characteristics.
Language: Английский
Citations
0Physics of Fluids, Journal Year: 2025, Volume and Issue: 37(1)
Published: Jan. 1, 2025
This paper proposes a fast and accurate method for predicting multi-row cascade flow based on framework of combined neural networks. The primary idea this is to decompose the whole-annulus into different types sub-regions, prediction surrogate models networks are constructed these sub-regions in rectangular computational domain by applying coordinate transformation technique. each sub-region then combined, continuity at interfaces among used iteratively compute cascade. main advantages proposed include reduced dataset generation cost network training through spatial decomposition, as well ability achieve combining sub-regions. test case two-dimensional stator-rotor interaction indicates that time developed approximately 5% required numerical simulation, with over 99% nodes field exhibiting normalized absolute error less than 0.05. approach can be further extended three-dimensional multi-stage turbomachinery.
Language: Английский
Citations
0Physics of Fluids, Journal Year: 2025, Volume and Issue: 37(1)
Published: Jan. 1, 2025
This paper introduces hydrological computational fluid dynamics model (HydroCFD), a deep learning based on the convolutional neural network U-Net framework designed for reconstructing free surface flow fields. With well-posed boundary and initial conditions, rapidly generates result that approximates two-dimensional (2D) shallow water equations, significantly improving efficiency of obtaining fields compared to traditional methods. The features an input layer integrates depth terrain (hydrological element variables), incorporates new loss function, coefficient variation function (CVLoss), improve accuracy stability. HydroCFD is trained validated two different datasets, open channel flows with groin, abrupt expansion. Error analysis demonstrated achieves high precision in 2D Furthermore, comparison six functions reveals CVLoss contributes improved
Language: Английский
Citations
0Aerospace Science and Technology, Journal Year: 2025, Volume and Issue: unknown, P. 109990 - 109990
Published: Jan. 1, 2025
Language: Английский
Citations
0Physics of Fluids, Journal Year: 2025, Volume and Issue: 37(2)
Published: Feb. 1, 2025
Repeatedly solving flow around structures with varying parameters using computational fluid dynamics (CFD) is often essential for structural design. This study proposes a boundary-assimilation Fourier neural operator (BAFNO) method to address the challenges of manually setting initial conditions CFD. The focus BAFNO on generalization ability predict fields without relying observational data. addresses boundary constraint requirements existing physics-informed models in parametric geometries. Inspired by ghost node method, domain are assimilated into loss function instead adding penalty terms. Meanwhile, structure boundaries damping source term level set function. can flexibly handle geometries different shapes and quantities. Subsequently, series numerical experiments flow-around conducted confirm performance BAFNO. results indicate that has strong capability, + CFD obtain dynamic stable faster than direct
Language: Английский
Citations
0Journal of Fluid Mechanics, Journal Year: 2025, Volume and Issue: 1007
Published: March 12, 2025
In this paper, the reflection of shock waves with downstream expansion fan interference in two-dimensional, inviscid flow is investigated, including steady Mach (MR) and unsteady transition process from regular (RR) to MR. A threshold for configuration based on non-dimensional wedge length proposed. The analytical model MR RR $\rightarrow$ established classical wave relations, whose prediction agrees well results obtained through numerical simulation. It found that significantly influences patterns, especially height stem shape slip line. interaction accelerates formation sonic throat, stabilizing structure rapidly, generally small heights. exposure triple point eliminates inflection line, slope increases smoothly. further affects time evolution during multiple-interaction stage process. appears modifications come curvature incident brought by interference. During stage, moves upstream along curved shock, where angle changes according curvature, resulting variation velocity.
Language: Английский
Citations
0Aerospace Science and Technology, Journal Year: 2025, Volume and Issue: unknown, P. 110194 - 110194
Published: April 1, 2025
Language: Английский
Citations
0Aerospace Science and Technology, Journal Year: 2025, Volume and Issue: unknown, P. 110287 - 110287
Published: May 1, 2025
Language: Английский
Citations
0Computers & Fluids, Journal Year: 2024, Volume and Issue: unknown, P. 106441 - 106441
Published: Sept. 1, 2024
Language: Английский
Citations
3Aerospace Science and Technology, Journal Year: 2025, Volume and Issue: unknown, P. 109917 - 109917
Published: Jan. 1, 2025
Language: Английский
Citations
0