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Author

Junqiang Bai

Bio: Junqiang Bai is an academic researcher from Northwestern Polytechnical University. The author has contributed to research in topics: Aerodynamics & Airfoil. The author has an hindex of 13, co-authored 91 publications receiving 505 citations.

Papers published on a yearly basis

Papers
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Journal ArticleDOI
TL;DR: In this article, a review of the recent advances of molecular simulation on gas adsorption/desorption and diffusion in the shale matrix is reviewed and further developments of the molecular simulation method in shale gas production are also discussed.
Abstract: Shale gas is becoming an increasingly promising alternative energy resource because of its high efficiency and environment-friendly characteristic. The amount of adsorbed gas on the shale matrix surfaces and dissolved gas in the shale matrix bulk is the dominant factor in the long-term productivity of shale reservoir. Although experimental measurements have been extensively carried out to investigate the gas adsorption and diffusion properties in the shale matrix, they cannot provide the detailed information on the microscopic transport mechanism of shale gas during the gas production process. Molecular simulation can accurately visualize the gas adsorption/desorption and diffusion processes in the shale matrix. In the present study, the recent research advances of molecular simulation on gas adsorption/desorption and diffusion in the shale matrix are reviewed. Firstly, the density functional theory (DFT) for shale gas molecule desorption/adsorption on the surface of the matrix crystal is illustrated. Then, the grand canonical Monte Carlo (GCMC) method predicting the amount of shale gas desorption/adsorption in the shale matrix crystal is introduced. Finally, molecular dynamics simulation (MD) for gas diffusion in the shale matrix is elucidated. Further developments of the molecular simulation method in shale gas production are also discussed.

95 citations

Journal ArticleDOI
TL;DR: This paper presents a data-driven approach for predicting the pressure distribution over airfoils based on Convolutional Neural Network (CNN), and utilizes a universal and flexible parametrization method called Signed Distance Function to improve the performances of CNN.

56 citations

Journal ArticleDOI
TL;DR: The results demonstrate that the gradient-based aero-stealth optimization design method can deal with the multidisciplinary optimization problems which require a large number of design variables.

52 citations

Journal ArticleDOI
TL;DR: In this paper, a grid strategy specific to structured grids for predicting the hypersonic aerodynamic heating loads is studied and the three-dimensional Navier-Stokes (NS) equations are simulated.

41 citations

Journal ArticleDOI
TL;DR: In this article, the thermal protection system combining the spike technology with the opposing jet technology is investigated and the three-dimensional compressible Reynolds Averaged Navier-Stokes (RANS) equations are simulated and Menter's shear stress transport (SST) turbulence model is applied.

37 citations


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04 Jun 2008
TL;DR: In this article, a coupling methodology between an upstream Reynolds Averaged Navier-Stokes (RANS) simulation and a large eddy simulation (LES) further downstream is presented.
Abstract: Abstract A coupling methodology between an upstream Reynolds Averaged Navier–Stokes (RANS) simulation and a Large Eddy Simulation (LES) further downstream is presented. The focus of this work is on the RANS-to-LES interface inside an attached turbulent boundary layer, where an unsteady LES content has to be explicitly generated from a steady RANS solution. The performance of the Synthetic-Eddy Method (SEM), which generates realistic synthetic eddies at the inflow of the LES, is investigated on a wide variety of turbulent flows, from simple channel and square duct flows to the flow over an airfoil trailing edge. The SEM is compared to other existing methods of generation of synthetic turbulence for LES, and is shown to reduce substantially the distance required to develop realistic turbulence downstream of the inlet.

180 citations

Journal ArticleDOI
TL;DR: A comprehensive and state-of-the art survey on common surrogate modeling techniques and surrogate-based optimization methods is given, with an emphasis on models selection and validation, dimensionality reduction, sensitivity analyses, constraints handling or infill and stopping criteria.

174 citations

Journal ArticleDOI
TL;DR: In this paper, a review of the shale gas transport process during shale gas production is presented, and the corresponding multi-scale simulation models that describe the gas multiscale transport mechanisms and accurately predict the amount of shale production are explained.

137 citations

Journal ArticleDOI
TL;DR: In this article, the authors provide a comprehensive understanding of the preparation and anti-icing applications of the super-hydrophobic coatings applied on the surface of aircrafts, and discuss the current research progress on the wetting theories of superhydrophobicity.
Abstract: Aircraft icing refers to ice formation and accumulation on the windward surface of aircrafts. It is mainly caused by the striking of unstable supercooled water droplets suspended in clouds onto a solid surface. Aircraft icing poses an increasing threat to the safety of flight due to the damage of aerodynamic shape. This review article provides a comprehensive understanding of the preparation and anti-icing applications of the superhydrophobic coatings applied on the surface of aircrafts. The first section introduces the hazards of aircraft icing and the underlying formation mechanisms of ice on the surface of aircrafts. Although some current anti-icing and de-icing strategies have been confirmed to be effective, they consume higher energy and lead to some fatigue damages to the substrate materials. Considering the icing process, the functional coatings similar to lotus leaf with extreme water repellency and unusual self-cleaning properties have been proposed and are expected to reduce the relied degree on traditional de-icing approaches and even to replace them in near future. The following sections mainly discuss the current research progress on the wetting theories of superhydrophobicity and main methods to prepare superhydrophobic coatings. Furthermore, based on the bouncing capacity of impact droplets, the dynamic water repellency of superhydrophobic coatings is discussed as the third evaluated parameter. It is crucial to anti-icing applications because it describes the ability of droplets to rapidly bounce off before freezing. Subsequently, current studies on the application of anti-icing superhydrophobic coatings including the anti-icing mechanisms and application status are introduced in detail. Finally, some limitations and issues related to the anti-icing applications are proposed to provide a future outlook on investigations of the superhydrophobic anti-icing coatings.

103 citations