Xin Yan

ORCID: 0000-0001-6143-9795
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About
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Research Areas
  • Tribology and Lubrication Engineering
  • Turbomachinery Performance and Optimization
  • Heat Transfer Mechanisms
  • Aerodynamics and Fluid Dynamics Research
  • Fluid Dynamics and Turbulent Flows
  • Hydraulic and Pneumatic Systems
  • Gear and Bearing Dynamics Analysis
  • Natural Language Processing Techniques
  • Topic Modeling
  • Computational Fluid Dynamics and Aerodynamics
  • Heat Transfer and Boiling Studies
  • Heat Transfer and Optimization
  • Text and Document Classification Technologies
  • Fluid Dynamics and Vibration Analysis
  • Mechanical stress and fatigue analysis
  • Advanced Text Analysis Techniques
  • Combustion and flame dynamics
  • Magnetic Bearings and Levitation Dynamics
  • Advanced Computational Techniques and Applications
  • Heat transfer and supercritical fluids
  • Cavitation Phenomena in Pumps
  • Educational Technology and Assessment
  • Data Visualization and Analytics
  • Nuclear Engineering Thermal-Hydraulics
  • Sentiment Analysis and Opinion Mining

Kunming University of Science and Technology
2013-2025

Xi'an Jiaotong University
2015-2024

Nanjing University of Posts and Telecommunications
2024

Changsha University of Science and Technology
2021-2024

Northeastern University
2021

Shanghai Electric (China)
2019

Sun Yat-sen University
2015

Institute of Flight
2014

Naval University of Engineering
2012

Pennsylvania State University
2011-2012

10.1016/j.ijheatmasstransfer.2023.124734 article EN International Journal of Heat and Mass Transfer 2023-09-28

Abstract A numerical method using the multiple frequencies elliptical whirling orbit model and transient Reynolds-averaged Navier–Stokes (RANS) solution was proposed for prediction of frequency dependent rotordynamic coefficients annular gas seals. The excitation signal waveform that acts as motion rotor center. RANS combined with mesh deformation utilized to solve leakage flow field in seal obtain response forces on surface. Frequency were determined by transforming dynamic monitoring data...

10.1115/1.4023143 article EN Journal of vibration and acoustics 2013-03-28

10.1016/j.ijheatmasstransfer.2017.08.090 article EN International Journal of Heat and Mass Transfer 2017-09-04

Numerical investigations on the rotordynamic characteristics of a typical hole-pattern seal using transient three-dimensional Reynolds-averaged Navier–Stokes (RANS) solution and periodic circular orbit model were conducted in this work. The unsteady solutions combined with mesh deformation method utilized to solve RANS equations obtain reaction forces rotor at five different excitation frequencies. relation between frequency dependent coefficients was obtained by considering (including...

10.1115/1.4003403 article EN Journal of vibration and acoustics 2011-04-08

Effects of pressure ratio and rotational speed on the leakage flow cavity characteristics rotating staggered labyrinth seal were investigated by means experimental measurements numerical simulations. The test rig with turbine flowmeter measuring instruments was utilized to investigate at eight ratios five speeds. repeatability data demonstrated three times different fixed speed. three-dimensional Reynolds-averaged Navier–Stokes equations standard k-ε turbulent model also applied study...

10.1115/1.4003788 article EN Journal of Engineering for Gas Turbines and Power 2011-05-18

Abstract Three-dimensional Reynolds-averaged Navier–Stokes (RANS) solutions from CFX were utilized to investigate the leakage flow characteristics in labyrinth honeycomb seal of steam turbines. At first, accuracy and reliability RANS approach was demonstrated using published experimental data seal. It showed that numerical method has sufficient precision predict performance seals. Then a range sealing clearances, cell diameters, depths, rotation speeds, pressure ratios investigated determine...

10.1115/1.4000091 article EN Journal of Engineering for Gas Turbines and Power 2010-03-16

The project review information plays an important role in the recommendation of experts. In this paper, we aim to determine expert's rating by using historical records and final decision results on previous projects, means some rules, construct a matrix for projects For data sparseness problem "cold start" new expert recommendation, assume that those projects/experts with similar topics have feature vectors propose collaborative algorithm based topic relationship. Firstly, obtain latent...

10.1109/jas.2015.7296535 article EN IEEE/CAA Journal of Automatica Sinica 2015-10-10

Tooth bending damage resulting from an intense impact by the rotor sometimes occurs in transient operation. To investigate influence of after-damage clearance and tooth length on leakage performance rotordynamic coefficients labyrinth seals, three damages were taken into consideration, including unbent (abbreviated as Unbent), partial Pbent) complete Cbent). The CFD solution was utilized to calculate flow rates seals with clearances 0.3, 0.4, 0.5, 0.6 mm for damages. obtained result shows...

10.1016/j.cja.2019.12.004 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2020-02-12

10.1016/j.ijheatmasstransfer.2012.03.045 article EN International Journal of Heat and Mass Transfer 2012-05-25

Spectral proper orthogonal decomposition (SPOD) is performed to identify the spatiotemporal coherent structures of trailing edge cutback film cooling flows. The analyzed data obtained from delayed-detached eddy simulation are validated against experimental first, followed by extraction SPOD modes and reconstruction flow fields using modes. Results show that topology flows mainly determined blowing ratio. At low ratios, vortex shedding phenomenon captured first leading mode. Its mode shape...

10.1063/5.0098796 article EN Physics of Fluids 2022-09-12

Abstract The viscous work generated by the rotating components of a seal not only represents direct loss power but also causes an increase in total temperature fluid (windage effect). In order to study discharge and characteristics stepped labyrinth seals with smooth honeycomb lands, 3D Reynolds-averaged Navier–Stokes solutions from CFX is used this work. At first, influences inlet preswirl, leakage flow rate, rotational speed on convergent divergent lands are conducted. obtained numerical...

10.1115/1.3068320 article EN Journal of Turbomachinery 2009-07-02

Three-dimensional Reynolds-averaged Navier–Stokes solutions are employed to investigate the discharge and total temperature increase characteristics of stepped labyrinth seal with honeycomb land. First, relations between windage heating number circumferential Mach at different Reynolds numbers for seals calculated compared experimental data. The obtained numerical results show that present three-dimensional periodic model can properly predict in seals. Then, a range pressure ratios, three...

10.1115/1.4001296 article EN Journal of Engineering for Gas Turbines and Power 2010-08-30

Brush seals have found increasing use in turbomachinery within the past decade due to their superior sealing performance and flexible nature. The flow characteristics fundamental behavior of single brush seal are known. However, multi-stage combined with labyrinth teeth still requires further research. This article presents a detailed investigation into for turbine applications. leakage rate through two-stage was measured using rotating test rig at three operating clearances four rotational...

10.1177/0957650914522456 article EN Proceedings of the Institution of Mechanical Engineers Part A Journal of Power and Energy 2014-02-03

To support the knowledge discovery and decision making from large-scale, multi-dimensional, continuous data sets, novel systems of visual analytics need capability to identify hidden patterns in that are critical for in-depth analysis. In this paper, we present a work-centered approach complex sets by combining user-centered interactive visualization data-oriented computational algorithms. We design implement specific system prototype, Learning-based Interactive Visualization Engineering...

10.1109/hicss.2012.87 article EN 2012-01-01
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