Weiwei Hui

ORCID: 0000-0001-7726-6681
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About
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Research Areas
  • Plasma and Flow Control in Aerodynamics
  • Aerodynamics and Fluid Dynamics Research
  • Fluid Dynamics and Turbulent Flows
  • Bioinformatics and Genomic Networks
  • Plasma Applications and Diagnostics
  • Surface Modification and Superhydrophobicity
  • Plasma Diagnostics and Applications
  • Icing and De-icing Technologies
  • Rocket and propulsion systems research
  • Biomedical Text Mining and Ontologies
  • Gene expression and cancer classification
  • Computational Drug Discovery Methods
  • Energetic Materials and Combustion
  • MicroRNA in disease regulation
  • Aerosol Filtration and Electrostatic Precipitation
  • RNA modifications and cancer
  • Cancer-related molecular mechanisms research
  • Thermal and Kinetic Analysis
  • Mechanical Behavior of Composites
  • Neonatal Health and Biochemistry
  • Lattice Boltzmann Simulation Studies
  • High-Velocity Impact and Material Behavior
  • Cytomegalovirus and herpesvirus research
  • Carbon Nanotubes in Composites
  • Machine Learning in Bioinformatics

Northwestern Polytechnical University
2017-2023

China Aerodynamics Research and Development Center
2022

China Mobile (China)
2020

China International Science and Technology Cooperation
2019

Children's Hospital of Chongqing Medical University
2019

Chongqing Medical University
2019

Abstract Motivation A microRNA (miRNA) is a type of non-coding RNA, which plays important roles in many biological processes. Lots studies have shown that miRNAs are implicated human diseases, indicating might be potential biomarkers for various types diseases. Therefore, it to reveal the relationships between and diseases/phenotypes. Results We propose novel learning-based framework, MDA-CNN, miRNA-disease association identification. The model first captures interaction features diseases...

10.1093/bioinformatics/btz254 article EN Bioinformatics 2019-04-06

Gene Ontology (GO) is one of the most popular bioinformatics resources. In past decade, Ontology-based gene semantic similarity has been effectively used to model gene-to-gene interactions in multiple research areas. However, existing approaches rely only on GO annotations and structure, or incorporate local co-functional network. This may lead inaccurate GO-based resulting from incomplete topology structure annotations.We present NETSIM2, a new network-based method that allows researchers...

10.1186/s12918-018-0539-0 article EN BMC Systems Biology 2018-03-01

The Gene Ontology (GO) is a community-based bioinformatics resource that employs ontologies to represent biological knowledge and describes information about gene product function. GO includes three independent categories: molecular function, process cellular component. For better reasoning, identifying the relationships between terms in different categories are important. However, existing measurements calculate similarity either developed by using data only or take part of combined...

10.1186/s12859-017-1959-3 article EN cc-by BMC Bioinformatics 2017-12-01

Recently, measuring phenotype similarity began to play an important role in disease diagnosis. Researchers have begun pay attention develop measurement. However, existing methods ignore the interactions between phenotype-associated proteins, which may lead inaccurate similarity. We proposed a network-based method PhenoNet calculate phenotypes. localized phenotypes network and calculated modules by modeling both inter- intra-similarity. was evaluated on two independent evaluation datasets:...

10.1186/s12859-018-2102-9 article EN cc-by BMC Bioinformatics 2018-04-01

The coupling characteristics of the aerodynamic and thermal effects a surface dielectric barrier discharge plasma actuator its transfer in different boundary-layer flows are studied experimentally. is attached to flat-plate airfoil driving by an alternative-current signal. Different achieved wind tunnel adjusting airfoil's angle attack with Reynolds number 2.02 × 105. spatial temperature-rise distributions velocity fields induced actuation quiescent air show that influence range temperature...

10.1063/5.0084420 article EN Physics of Fluids 2022-03-01

A pair of surface mounted dielectric-barrier-discharge (DBD) plasma actuators is placed diametrically on a circular cylinder model. The flow field generated by the in steady and duty-cycle actuation modes measured particle image velocimetry. Salient features vortices are discovered for with frequency ranging from 5 to 1000 Hz ratio 0.01 0.99. results compared those continuous actuation. For given ratio, discrete vortex each DBD actuator an cycle low frequencies. Such created alternately side...

10.1063/5.0124744 article EN Physics of Fluids 2022-12-01

Abstract Motivation A microRNA (miRNA) is a type of non-coding RNA, which plays important roles in many biological processes. Lots studies have shown that miRNAs are implicated human diseases, indicating might be potential biomarkers for various types diseases. Therefore, it to reveal the relationships between and diseases/phenotypes. Results We propose novel learning-based framework, MDA-CNN, miRNA-disease association identification. The model first captures richer interaction features...

10.1101/276048 preprint EN bioRxiv (Cold Spring Harbor Laboratory) 2018-03-06

The Human Phenotype Ontology (HPO) is one of the most popular bioinformatics resources. Recently, HPO-based phenotype semantic similarity has been effectively applied to model patient data. However, existing tools are revised based on Gene (GO)-based term similarity. design models not optimized for unique features HPO. In addition, only allow HPO terms as input and provide pure text-based outputs.We present PhenoSimWeb, a web application that allows researchers measure similarities using...

10.1186/s12864-018-4927-z article EN cc-by BMC Genomics 2018-08-01

A NACA0025 coflow jet airfoil model, including the inner and outer airfoils, was designed manufactured through 3D printing technology. Using duct connecting leading- trailing-edge slots formed by eight plasma actuators are arranged in synchronously driven two high-voltage alternating-current sources to realize (PCFJ) flow control technique. The test angle of attack range is 8–30°, Reynolds number 68,000. induced airflow characteristics were studied, mechanism PCFJ explored using detailed...

10.2514/1.j060911 article EN AIAA Journal 2021-10-26

As one of the key components solid rocket motors (SRMs) and launch vehicles (LVs), deformation damage composite motor case (CRMC) can directly affect effectiveness SRMs. Therefore, it is particularly important to analyze failure cases. analysis remains complex due different modes composites at scales, this paper applies multiscale methods CRMC damage. A mechanical model established, data transfer between microscale, mesoscale, macroscale models achieved using submodel techniques. In paper,...

10.3389/fmats.2023.1198493 article EN cc-by Frontiers in Materials 2023-06-02

Download This Paper Open PDF in Browser Add to My Library Share: Permalink Using these links will ensure access this page indefinitely Copy URL DOI

10.2139/ssrn.4771795 preprint EN 2024-01-01

Recently, measuring phenotype similarity began to play an important role in disease diagnosis. Researchers have begun pay attention develop measurement. However, existing methods ignore the interactions between phenotype-associated proteins, which may lead inaccurate similarity. We proposed a network-based method PhenoNet calculate phenotypes. localized phenotypes network and calculated modules by modeling both inter- intra-similarity. was evaluated on two independent evaluation datasets:...

10.1109/bibm.2017.8217911 article EN 2021 IEEE International Conference on Bioinformatics and Biomedicine (BIBM) 2017-11-01

Abstract The significance of the mechanical properties solid propellant during curing process lies in their contribution to stress‐strain calculations viscoelastic engineering materials and analysis structural integrity rocket motor charges. In order study Constitutive equation nitrate ester plasticized polyether (NEPE) process, indentation creep tests were carried out on NEPE propellant, constitutive model with reaction at 50 °C atmospheric pressure was studied. Firstly, based theory,...

10.1002/prep.202300169 article EN Propellants Explosives Pyrotechnics 2023-10-24

Surface Dielectric Barrier Discharge (SDBD) plasma actuators driven by alternating current (AC), also known as AC-SDBD, have been used recently in many aerodynamic and heat transfer applications. The present study investigates experimentally the thermal effects of AC-SDBD actuator presence an external flow i.e. wind tunnel. oil visualization infrared thermography is performed to determine different boundary layer regions over model properties placed on upper surface, respectively. tunnel...

10.2514/6.2020-3228 article EN AIAA Aviation 2019 Forum 2020-06-08

To establish a stable HEK293T cell line with c.392G>T (p.131G>V) mutation site knockout in

10.12122/j.issn.1673-4254.2019.03.10 article EN PubMed 2019-03-30

View Video Presentation: https://doi.org/10.2514/6.2022-3875.vid The new concept of the anti-/de-icing method based on Alternative-Current high voltage-driven surface dielectric barrier discharge (AC-SDBD) plasma actuation has no complicated mechanical structure and potential aerodynamic loss, making it to be anti- de-icing methods used by next-generation aircraft. AC-SDBD will produce thermal, aerodynamic, chemical electromagnetic effects, etc. Existing studies have shown that coupling...

10.2514/6.2022-3875 article EN AIAA Aviation 2019 Forum 2022-06-20

View Video Presentation: https://doi.org/10.2514/6.2023-4434.vid The anti-/de-icing method based on Surface Dielectric Barrier Discharge plasma actuation driven by AC high-voltage signal has no complex mechanical structure and potential aerodynamic loss, which makes it a for the next generation of aircraft. existing research shows that coupling multiple physical fields causes effect supercooled water droplets. Meanwhile, this occurs in different time scales, is challenging its research. In...

10.2514/6.2023-4434 article EN AIAA Aviation 2019 Forum 2023-06-08

View Video Presentation: https://doi.org/10.2514/6.2023-3777.vid Alternative-Current high voltage-driven surface dielectric barrier discharge (AC-SDBD) plasma actuation is a new concept of the anti-/de-icing method with no complicated mechanical structure and potential aerodynamic loss, which makes it to be anti- de-icing methods used by next-generation aircraft. AC-SDBD has not only effects, but also thermal, chemical electromagnetic etc. Many studies have shown that coupling...

10.2514/6.2023-3777 article EN AIAA Aviation 2019 Forum 2023-06-08

Detailed two-dimensional particle image velocimetry (2D-PIV) is presented to study the vortex flow behind a cylindrical model with plasma control. A pair of alternating-current surface-dielectric-barrier-discharge (AC-SDBD) actuators symmetrically placed at azimuth angles ±90 degrees on surface. The asymmetric near cylinder visualized and measured steady unsteady actuation respectively in an open-test section return-circuit low-speed wind tunnel. incoming 5 m/s Reynolds number based diameter...

10.2514/6.2020-2958 article EN AIAA Aviation 2019 Forum 2020-06-08

Flow control based on AC-SDBD plasma actuators has been widely used in various research regions of aerodynamics. However, the drawback flow is low efficiency energy conversion. It means induced aerodynamic effect only consumes a small part total electrical power, and large converted into heat with an obvious thermal effect, which often ignored by researchers. Our team proposed concept icing recent years engage new study: coupling effects effects. In this study, transfer characteristics...

10.2514/6.2022-2592 article EN AIAA SCITECH 2022 Forum 2022-01-03

When an aircraft flies through icy cloud at a low altitude and with speed, the surface of its windward parts will freeze due to impact supercooled water droplets in cloud. key aerodynamic parts, including leading-edge wings propeller blades, other are frozen, it seriously affect shape result drag increase lift reduction. It also controllability stability cause serious safety accidents. Therefore, icing phenomenon airplanes flight corresponding mechanism have always been focus attention by...

10.2514/6.2022-2594 article EN AIAA SCITECH 2022 Forum 2022-01-03

View Video Presentation: https://doi.org/10.2514/6.2022-3850.vid A circular cylinder using Plasma Co-Flow Jet (PCFJ) flow control technique was designed and manufactured through 3D printing technology. pair of PCFJ actuators are symmetrically distributed at ±90° azimuth angles. One actuator includes 4 long strips plasma to achieve the blowing suction effects realize co-flow jet technique. The near-field vortices were visualized a detailed particle-image-velocimetry (PIV) spatial dynamic...

10.2514/6.2022-3850 article EN AIAA Aviation 2019 Forum 2022-06-20
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