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Journal ArticleDOI

Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded high-speed aerodynamic flows

TLDR
In this article, the authors performed an experimental analysis of base pressure in suddenly expanded compressible flow from nozzles at different Mach numbers and found that microjets are efficient when the flow is under the influence of a favorable pressure gradient.
About
This article is published in Aerospace Science and Technology.The article was published on 2020-12-01. It has received 66 citations till now. The article focuses on the topics: Adverse pressure gradient & Mach number.

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Citations
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A novel hybrid method for flight departure delay prediction using Random Forest Regression and Maximal Information Coefficient

TL;DR: The proposed RFR-MIC model exhibits good performance compared with linear regression, k-nearest neighbors, artificial neural network, and standard Random Forest Regression, and the results show that flight information on multiple air routes can certainly improve the accuracy of flight departure delay prediction.
Journal ArticleDOI

Power plant energy predictions based on thermal factors using ridge and support vector regressor algorithms

TL;DR: In this paper, a combined cycle power plant (CCPP) was modeled using different algorithms, including Ridge, Linear Regression (LR), Support Vector Regressor (SVR), and Upport vector Regressor(SVR).
Journal ArticleDOI

Finding the optimal design of a Cantor fractal-based AC electric micromixer with film heating sheet by a three-objective optimization approach

TL;DR: In this article , a three-objective optimization process for an Alternating Current (AC) electrothermal theory-based micromixer is presented, in which the width-to-length ratio (a/b) of the AC electrode based on the Cantor fractal, the inlet velocity (U), the voltage amplitude (V), and the heat of the film heating sheet (Q) are design variables.
References
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Journal ArticleDOI

Physics-informed neural networks for high-speed flows

TL;DR: In this article, a physics-informed neural network (PINN) was used to approximate the Euler equations that model high-speed aerodynamic flows in one-dimensional and two-dimensional domains.
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Aircraft viscous drag reduction using riblets

TL;DR: In this paper, the performance of 3 M riblets on airfoils, wings and wing-body or aircraft configurations at different speed regimes are reviewed; these applications bring in additional effects like pressure gradients and three dimensionality.
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Machine learning methods for turbulence modeling in subsonic flows around airfoils

TL;DR: In this article, a high Reynolds number turbulent flows around the airfoils and the results calculated by the computational fluid dynamics solver with the Spallart-Allmaras (SA) model were used as training data to construct a high-dimensional data-driven network model based on machine learning.
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Development and Verification of an Online Artificial Intelligence System for Detection of Bursts and Other Abnormal Flows

TL;DR: The objective of the work presented in this paper was to assess the online application and resulting benefits of an artificial intelligence system for detection of leaks/bursts at district meter area (DMA) level.
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Computational Fluid Dynamics in Turbomachinery: A Review of State of the Art

TL;DR: In this article, the authors reviewed the state of the art work carried out in the field of turbomachinery using computational fluid dynamics (CFD) and highlighted the prevailing merits and demerits of CFD in turbomachines.
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