Heat Transfer, Combustion and Flow Dynamics in Propulsion Systems

Propulsion systems based on chemical reaction principles are still the most widely used thrust devices for aircrafts, drawing a lot of research attention. Whether in traditional propulsion systems including aero-engines, rocket engines, ramjets and scramjets, or new developed combined power systems...

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Bibliographic Details
Format: eBook
Language:English
Published: Basel MDPI - Multidisciplinary Digital Publishing Institute 2023
Subjects:
PIV
Online Access:Open Access: DOAB: description of the publication
Open Access: DOAB, download the publication
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720 1 |a Liu, Jian  |4 edt 
720 1 |a Fu, Qingfei  |4 edt 
720 1 |a Fu, Qingfei  |4 oth 
720 1 |a Liu, Chaoyang  |4 edt 
720 1 |a Liu, Chaoyang  |4 oth 
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720 1 |a Tong, Yiheng  |4 edt 
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245 0 0 |a Heat Transfer, Combustion and Flow Dynamics in Propulsion Systems 
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520 |a Propulsion systems based on chemical reaction principles are still the most widely used thrust devices for aircrafts, drawing a lot of research attention. Whether in traditional propulsion systems including aero-engines, rocket engines, ramjets and scramjets, or new developed combined power systems (such as TBCCs and RBCCs), thermal protection, flow dynamics and combustion instabilities in engine systems are still major concerns, especially for high-speed aircraft. Thermal protection has become the biggest issue for hypersonic aircraft experiencing extremely high external aerodynamic heating and internal combustion heat release. Another challenging issue is the risk of combustion instability inside some propulsion systems, which couples with an unsteady heat release process and leads to high thermal load. Some optimized or novel design, analysis and simulated methods have been applied to the structural design, heat transfer and flow dynamics of propulsion systems. New measurement methods have been proposed to realize clear and accurate visualizations of flow field and combustion products, such as high-resolution PIV and burst-mode high frequency LIF. In addition, new concepts have been proposed aiming at improving the efficiency of propulsion systems, such as the application of powder fuel instead of traditional fuels and the application of supercritical fluids and nanofluids in thermal management systems. 
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650 7 |a History of engineering and technology  |2 bicssc 
650 7 |a Technology: general issues  |2 bicssc 
653 |a acceleration 
653 |a acoustic oscillations 
653 |a additive manufacturing 
653 |a ammonia fuel 
653 |a asymmetric heating 
653 |a atomization characteristics 
653 |a C-X CH PLIF 
653 |a chamber backpressure 
653 |a chirality 
653 |a closed flame system 
653 |a coolant coverage 
653 |a critical heat flux 
653 |a cryogenic flow boiling 
653 |a departure from nucleate boiling correlation 
653 |a dynamic characteristics 
653 |a endwall film cooling 
653 |a extreme turbulence 
653 |a flow pattern 
653 |a gas-centered swirl coaxial injector 
653 |a gelled fuel 
653 |a GR-Cop42 
653 |a heat and mass transfer 
653 |a heat flux 
653 |a heat transfer enhancement 
653 |a Kelvin-Helmholtz instability 
653 |a liquid film 
653 |a multiphysics field simulation 
653 |a non-circular channels 
653 |a nonlinear dynamic analysis 
653 |a PIV 
653 |a porous/lattice structures 
653 |a premixed combustion 
653 |a pressure measurement 
653 |a pulsation flow 
653 |a regenerative cooling 
653 |a rheological properties 
653 |a Sauter mean diameter 
653 |a shipborne UAV applications 
653 |a solid oxide fuel cell 
653 |a spatial orthogonal bifurcation 
653 |a supercritical CO2 
653 |a thermal management technology 
653 |a thermophysical property 
653 |a transpiration cooling 
653 |a tubular structure 
653 |a turbine vane 
653 |a vortex structure 
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856 4 0 |u https://mdpi.com/books/pdfview/book/8156  |7 0  |z Open Access: DOAB, download the publication