Ting Wang

ORCID: 0000-0001-8222-9076
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About
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Research Areas
  • Fluid Dynamics and Turbulent Flows
  • Heat Transfer Mechanisms
  • Combustion and flame dynamics
  • Turbomachinery Performance and Optimization
  • Aerodynamics and Acoustics in Jet Flows
  • Thermochemical Biomass Conversion Processes
  • Wind and Air Flow Studies
  • Numerical methods in inverse problems
  • Sparse and Compressive Sensing Techniques
  • Granular flow and fluidized beds
  • Fire dynamics and safety research
  • Gas Dynamics and Kinetic Theory
  • Particle Dynamics in Fluid Flows
  • Fluid Dynamics and Heat Transfer
  • Heat transfer and supercritical fluids
  • Fluid Dynamics and Vibration Analysis
  • Nanofluid Flow and Heat Transfer
  • Radiative Heat Transfer Studies
  • Heat Transfer and Numerical Methods
  • Cyclone Separators and Fluid Dynamics
  • Fluid Dynamics and Thin Films
  • Photoacoustic and Ultrasonic Imaging
  • Human Motion and Animation
  • 3D Shape Modeling and Analysis
  • Advanced Optimization Algorithms Research

Xi’an University of Posts and Telecommunications
2023-2024

University of New Orleans
2010-2023

Nanjing Tech University
2022

Zhejiang Sci-Tech University
2021

City University of Hong Kong
2021

Harbin Electric Corporation (China)
2021

Guilin University of Technology
2021

Northeast Electric Power University
2018

Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
2014

Institute of Software
2008

10.1016/j.ijheatmasstransfer.2009.12.047 article EN International Journal of Heat and Mass Transfer 2010-02-04

10.1016/j.ijheatmasstransfer.2020.120197 article EN International Journal of Heat and Mass Transfer 2020-07-25

Numerical simulation is performed in this study to explore film-cooling enhancement by injecting mist into the cooling air with a focus on investigating effect of various modeling schemes results. The turbulence models, dispersed-phase modeling, inclusion different forces (Saffman, thermophoresis, and Brownian), trajectory tracking, injection scheme studied. flow inlet boundary conditions (with/without supply plenum), intensity, near-wall grid density results also included. Simulation...

10.1115/1.2709959 article EN Journal of Heat Transfer 2007-01-03

When pulling a particle in driven granular fluid with constant force $F_{ex}$, the probe approaches steady-state average velocity $v$. This and corresponding friction coefficient of $\zeta=F_{ex}/v$ are obtained within schematic model mode-coupling theory compared to results from event-driven simulations. For small moderate drag forces, describes simulation successfully for both linear as well nonlinear region: The response regime (constant friction) forces is followed by shear thinning...

10.1103/physreve.89.042209 article EN Physical Review E 2014-04-28

The output and efficiency of gas turbines are reduced significantly during the summer. Gas turbine inlet air-cooling is considered a simple effective method to increase power as well thermal efficiency. Among various cooling schemes, fog (a direct evaporative cooling) has gained increasing popularity due its simplicity low installation cost. During cooling, water atomized micro-scaled droplets (or mist) introduced into airflow. air temperature through evaporation. To investigate mist...

10.1080/10407780701790003 article EN Numerical Heat Transfer Part A Applications 2008-01-08

10.1016/0894-1777(95)00126-3 article EN Experimental Thermal and Fluid Science 1996-04-01

A stage-by-stage wet-compression theory and algorithm have been developed for overspray interstage fogging in the compressor. This are used to calculate performance of an 8-stage compressor under both dry wet compressions. 2D airfoil geometry stage setting at mean radius employed. Six different cases with without investigated compared. The pressure ratio enhances during all as does overall ratio, saturated (no overspray) achieving highest ratio. Saturated reduces specific work, but increases...

10.1115/gt2008-50323 article EN 2008-01-01

Compressor intercooling has traditionally been employed to reduce compressor work and augment gas turbine output power. Conventional schemes are usually applied through non-mixed heat exchangers between two stages or by cooling the outside of casing. Any that may affect flow field inside compressors have not favorably considered due concerns any disturbance might adversely compressor’s performance stability. As inlet fog scheme become popular as an economic effective means power on hot dry...

10.1115/gt2008-50322 article EN 2008-01-01

This first part of the paper presents techniques implemented for experimental investigation transition mechanism in 2-D pressure driven separated boundary layer flows over a flat plate at inlet free-stream turbulence intensities ranging from 0.3 to 0.6% and imposed adverse gradients K = − 0.68 × 10−6 6.25 10−6. The structure behavior separation bubble were investigated various flow conditions. separated-flow modes identified classified. distribution end strength gradient obtained by varying...

10.1115/98-gt-461 article EN Volume 1: Turbomachinery 1998-06-02

Purpose This study focused on how to realize automatic recognition of young women's neck-shoulder shape based the front and side images. Design/methodology/approach The reverse engineering software was used measure body sizes part three-dimensional (3D) point cloud data, important parameters closely related were determined. subjects classified establish classification rules. Then, images, human contour extracted by Matlab, data required for obtained identifying feature points. Findings...

10.1108/ijcst-05-2020-0079 article EN International Journal of Clothing Science and Technology 2021-03-30

This paper clearly identifies the possible modes of transition in separated boundary layers and their specific characteristics. study distinguishes between short long bubbles primarily based on flow structure. A hypothetical description vortex structure evolution for each separated-flow mode is provided. The present approach analyzing assumption that to turbulence a result superposition effects two different types instability. first type instability Kelvin-Helmholtz (KH) It occurs develops...

10.1115/98-gt-463 article EN Volume 1: Turbomachinery 1998-06-02

The output and efficiency of gas turbines are reduced significantly during the summer. Gas turbine inlet air-cooling is considered a simple effective method to increase power as well thermal efficiency. Among various cooling schemes, fog (a direct evaporative cooling) has gained increasing popularity due its simplicity low installation cost. During cooling, water atomized micro-scaled droplets (or mist) introduced into airflow. air temperature through evaporation. To investigate mist...

10.1115/imece2004-60133 article EN 2004-01-01

The passive sweeping jet fluidic oscillators are a promising potential candidate in heat transfer applications such as gas turbine cooling, electronic components and exchanger enhancement component. This review presents detailed discussion, summary, comparison of the studies on jets. Sweeping jets can be created by two different types (i.e., wall-attachment type interaction type). Those do not need moving part nor active control to create In type, fluid enters oscillator, fills cavity...

10.1615/interjenercleanenv.2022041464 article EN International Journal of Energy for a Clean Environment 2022-06-07

The present paper focuses on presenting the results of experimental investigation transition process in separated boundary layers a flat plate at zero incidence, with imposed adverse pressure gradients. combined effects Reynolds number and gradient strength mechanism, bubble geometry, bursting are studied. flow structures unsteady aspects associated separated-flow analyzed for three representative cases. Surface detailed layer measurements using hot-wire anemometry presented as mean rms...

10.1115/98-gt-462 article EN Volume 1: Turbomachinery 1998-06-02

The present study formulates an improved approach for analyzing separated-flow transition that differentiates between the process in boundary layers which are laminar at separation and those already transitional separation. paper introduces new parameters necessary classifying modes accounting concomitant evolution of separated shear layer average effect periodic bubble build-up vortex shedding. At least three positively distinguished: (a) separation, with starting upstream point developing...

10.1115/98-gt-237 article EN Volume 1: Turbomachinery 1998-06-02

A Phase Doppler Particle Analyzer (PDPA) system is employed to measure the two-phase mist flow behavior including velocity field, droplet size distribution, dynamics, and turbulence characteristics. Based on measurements made through PDPA, a projected profile describing how air-mist coolant jet spreads eventually blends into hot main proposed. This proposed found be well supported by measurement results of turbulent Reynolds stresses. The film envelope identified with shear layers...

10.1115/gt2013-94478 article EN 2013-06-03

Calcined coke is an important material for making carbon anodes smelting alumina to aluminum. Calcining energy intensive industry and a significant amount of heat wasted in the calcining process. Efficiently managing this resource tied profit margin survivability plant. To help improve efficiency process, 3D computational model developed gain insight thermal-flow combustion behavior calciner. Comprehensive models are employed simulate moving petcoke bed with moisture evaporation,...

10.1115/1.4002524 article EN Journal of Thermal Science and Engineering Applications 2010-06-01

The output and efficiency of gas turbines are reduced significantly during the summer, especially in areas where daytime temperature reaches as high 50°C. Gas turbine inlet fogging overspray has been considered a simple cost-effective method to increase power output. One most important issues related is determine effective location device by determining (a) how many water droplets actually evaporate effectively cool down air instead colliding on wall or coalescing draining out (i.e....

10.1115/gt2011-46809 article EN 2011-01-01
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