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Hui Tang

Researcher at Hong Kong Polytechnic University

Publications -  152
Citations -  3673

Hui Tang is an academic researcher from Hong Kong Polytechnic University. The author has contributed to research in topics: Synthetic jet & Coating. The author has an hindex of 28, co-authored 150 publications receiving 2513 citations. Previous affiliations of Hui Tang include University of Electronic Science and Technology of China & University of Houston.

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Simulation of natural convection and entropy generation of non-Newtonian nanofluid in a porous cavity using Buongiorno’s mathematical model

TL;DR: In this article, the authors analyzed the natural convection and entropy generation of non-Newtonian nanofluid, using the Buongiorno's mathematical model in a cavity in the presence of a uniform magnetic field has been analyzed by Finite Difference Lattice Boltzmann method.
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Preparation and characterization of HA microflowers coating on AZ31 magnesium alloy by micro-arc oxidation and a solution treatment

TL;DR: In this article, a micro-arc oxidation and a solution treatment on AZ31 magnesium alloy was used to improve the corrosion resistance of the MAO sample, by forming a barrier layer on the surface of MAO coating, and by penetrating into the outer layer of theMAO film, sealing the micropores and micro-cracks existed in MAO-ST coating.
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Towards the design of synthetic-jet actuators for full-scale flight conditions Part 1: The fluid mechanics of synthetic-jet actuators

TL;DR: In this paper, a 3-year research program aiming at establishing a capability based on a better understanding of the fluid mechanics of synthetic jets and an improved modelling capacity is reported. But the capability that allows the geometry and operating conditions of these devices to be designed and selected for maximum flow-control effectiveness in full-scale flight conditions has yet to be developed.
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Towards the design of synthetic-jet actuators for full-scale flight conditions : Part 2: Low-dimensional performance prediction models and actuator design method

TL;DR: A methodology for designing synthetic-jet actuators used for flow separation control at full-scale flight conditions is developed and is illustrated in the design of actuators for delaying flow separation on the leading and trailing edge devices of a typical commercial-aircraft wing at take-off conditions.