Special Issues

Heat and Mass Transfer in Aero-Engines and Gas Turbines

Submission Deadline: 31 October 2026 View: 1203 Submit to Special Issue

Guest Editor(s)

Prof. Zhongyi Wang

Email: b205030024@126.com

Affiliation: College of Power and Energy Engineering, Harbin Engineering University, Harbin, 150001, China

Homepage:

Research Interests: complex multiphase and multiscale flow, heat and mass transfer theory, icing/anti-icing mechanism, advanced optical experimental testing technology

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Dr. Xiaohu Chen

Email: chen_xiaohu@hrbeu.edu.cn

Affiliation: College of Power and Energy Engineering, Harbin Engineering University, Harbin, 150001, China

Homepage:

Research Interests: theory of multiphase flow, heat and mass transfer mechanism, advanced cooling technology, thermal protection technology, particle deposition dynamics

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Dr. Yanhua Wang

Email: wangyanhua@hrbeu.edu.cn

Affiliation: College of Power and Energy Engineering, Harbin Engineering University, Harbin, 150001, China

Homepage:

Research Interests: droplet collision dynamics, icing/anti-icing theory, multiphase flow measurement and testing technology, multi-physical field coupling

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Dr. Meng Wang

Email: wangmeng_a@hrbeu.edu.cn

Affiliation: College of Power and Energy Engineering, Harbin Engineering University, Harbin, 150001, China

Homepage:

Research Interests: aerothermodynamics of turbomachinery, high-fidelity numerical calculation methods, multiphase flow measurement and testing technology, flow control mechanism, heat and mass transfer theory in compressors

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Summary

The performance boundaries of next-generation aero-engines and gas turbines, in their pursuit of higher efficiency, greater thrust, and lower emissions, are increasingly determined by breakthroughs in heat and mass transfer technologies. Efficient cooling under extreme thermal loads, reliable thermal protection, and the management of complex multiphase flows are critical to ensuring the operational safety and service life of core components. This special issue aims to collect high-quality manuscripts focusing on the forefront of this field, covering the full spectrum of innovation from fundamental theory to engineering applications. Topics include, but are not limited to: Fundamental theories and mechanisms of heat and mass transfer, multiphase flow, advanced cooling technologies, combustion theory, heat transfer enhancement mechanisms, thermal protection technologies, flow control and thermal management, as well as multi-physics and multi-scale simulations and advanced experimental testing technologies related to flow-heat transfer-mass transfer.


We particularly welcome original theories of heat and mass transfer, fundamental studies on heat and mass transfer mechanisms based on high-fidelity experiments and advanced numerical simulations, as well as innovative design concepts and research schemes that can effectively break through the bottlenecks in thermal efficiency, aerodynamic loss, cooling performance, combustion efficiency, heat exchange performance, icing/anti-icing performance, particle deposition and suppression performance, and component reliability.

Topics of interest include:

1. Fundamental theories and mechanisms of flow-heat-mass transfer under special/extreme operating conditions (e.g., heat and mass transfer in stationary/rotating components and inlet/exhaust systems, shock-wave/boundary-layer interactions, high/low altitude, sea salt aerosol, and sand-dust environments).

2. Flow-heat-mass transfer in key aero-engine/gas turbine components (e.g., flow control and heat-mass transfer in compressors, icing/anti-icing, flow-heat-mass transfer phenomena in combustors, film cooling, internal cooling, and conjugate heat transfer in turbine blades/vanes).

3. Multi-phase flow and heat-mass transfer (e.g., droplet/particle-laden flow and heat transfer, particle deposition, phase-change heat transfer, and multi-phase flow in combustors and heat exchangers).

4. Multi-physical field coupling of flow-heat-mass transfer (e.g., encompassing combustion chemistry and pollutant control, plasma actuation, and fluid-thermal-structural-chemical coupling inducing oxidation, corrosion, and performance degradation).

5. Numerical simulation and experimental measurement methods (e.g., heat-mass transfer models, high-fidelity numerical methods, multi-scale simulations, and advanced experimental techniques).

6. Optimization and control strategies (e.g., topology optimization, active/passive flow and heat transfer control, thermal management optimization, health management, and life assessment).

7. Emerging technologies and frontier issues (e.g., flow-heat-mass transfer in hypersonic propulsion systems, heat and mass transfer characteristics of alternative fuels in gas turbines, and phenomena in distributed propulsion/energy supply and hybrid power systems).


Keywords

aero-engine; gas turbine; turbulent flow; heat transfer; mass transfer; multiphase flow; multi-scale; multiphysics coupling; experimental testing techniques; numerical simulation; aerothermodynamics; compressor icing; anti-/de-icing; combustion; turbine cooling; film cooling; transpiration cooling; intake/exhaust system; conjugate heat transfer; particle deposition; thermal management; thermal protection; flow control; thermal barrier coatings; extreme environment; heat exchanger; structural optimization; hydrogen fuel; distributed energy

Published Papers


  • Open Access

    ARTICLE

    Effect of Surface Roughness on Flow Behavior and Conjugate Heat Transfer between TBC and Cooling Film

    Yuzhang Wang, Zhuning Liu, Haozhe Sun, Zhuo Li, Kanru Cheng, Chaoran Yang
    Frontiers in Heat and Mass Transfer, DOI:10.32604/fhmt.2026.084530
    (This article belongs to the Special Issue: Heat and Mass Transfer in Aero-Engines and Gas Turbines)
    Abstract During the operation of a gas turbine, the surface morphology of thermal barrier coatings (TBCs) of the high temperature blades inevitably evolves due to sintering, particle deposition or other factors, leading to an increase in surface roughness. This altered roughness can significantly influence the flow behavior of cooling films and the heat transfer performance of the coupled cooling film-TBC system. In this work, the flow behavior and conjugate heat transfer between cooling film and TBC under varying surface roughness conditions were investigated using the double distribution function lattice Boltzmann method (DDF-LBM) coupled with large eddy… More >

  • Open Access

    ARTICLE

    Dynamic Thermal Characteristics of Engine Oil Loop Integrated with Fuel Thermal Management

    Shiyu Yang, Yuanfang Lin, Yancong Qiao, Longfei Zhang, Haiyu Yu, Xianghua Xu, Xingang Liang
    Frontiers in Heat and Mass Transfer, DOI:10.32604/fhmt.2026.084170
    (This article belongs to the Special Issue: Heat and Mass Transfer in Aero-Engines and Gas Turbines)
    Abstract The rapid increase in onboard heat loads has made aircraft thermal management a critical issue. As an important part of the fuel thermal management system (FTMS), the dynamic thermal characteristics of the engine oil system (EOS) directly determine temperature regulation and fuel heat sink utilization, necessitating further investigation. In this paper, a novel dynamic heat transfer model for the oil pump was firstly developed through temperature step experiments. Subsequently, a transient flow and heat transfer model of the oil loop was established using the thermal fluid network (TFN) method, and the influence of thermal inertia… More >

    Graphic Abstract

    Dynamic Thermal Characteristics of Engine Oil Loop Integrated with Fuel Thermal Management

  • Open Access

    ARTICLE

    Thermomechanical Optimization Design of TGV Weight Respecting Restrictive Condition and Highly Sensitive Variables

    Peng Guan, Ming-Ran Li, Si-Bo-Wen Wang
    Frontiers in Heat and Mass Transfer, DOI:10.32604/fhmt.2026.082595
    (This article belongs to the Special Issue: Heat and Mass Transfer in Aero-Engines and Gas Turbines)
    Abstract This paper develops a thermomechanical optimization method for turbo guide vane (TGV) weight reduction under restrictive conditions and highly sensitive variables. The proposed method integrates a flow-thermo-structural model, orthogonal experimental design (OED), and an optimization framework based on response surface methodology (RSM) and a genetic algorithm (GA). To address both the plastic limit and temperature distribution of the TGV, a new parameter termed the stress ratio is introduced as a constraint during optimization. Six highly sensitive variables were selected from ten cooling channel diameters using OED. Simulation results based on the thermal-fluid coupling model were… More >

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