Advanced Propulsion System and Thermal Management Technology

The reprint focused on innovative developments in the fields of advanced propulsion system and thermal management technology. Propulsion systems develop along the direction of wide speed range and long endurance both for civil aircrafts and military applications. The research works of propulsion sys...

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Bibliographic Details
Other Authors: Liu, Jian (Editor), Liu, Chaoyang (Editor), Tong, Yiheng (Editor), Sunden, Bengt (Editor)
Format: Electronic Book Chapter
Language:English
Published: Basel MDPI - Multidisciplinary Digital Publishing Institute 2023
Subjects:
Online Access:DOAB: download the publication
DOAB: description of the publication
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245 1 0 |a Advanced Propulsion System and Thermal Management Technology 
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520 |a The reprint focused on innovative developments in the fields of advanced propulsion system and thermal management technology. Propulsion systems develop along the direction of wide speed range and long endurance both for civil aircrafts and military applications. The research works of propulsion systems mainly include overall design, combustion, aerodynamic, internal flows and heat transfer etc. High efficiency is pursed not only by optimized designs but also from development of materials as well as application of new fuel. Along with development of high efficiency propulsion system, thermal management technology is also developed to meet the demand of external aerodynamic heating and internal combustion heat at a high flight speed. Common thermal management technology includes blade cooling in gas turbines and regenerative cooling in rocket engines. Thermal protection of engines achieves high efficiency by heat transfer enhancement, such as use of superficial fluid, nanofluids and new designed roughened surfaces. Also, some heat transfer enhancement methods in heat exchangers, battery and fuel cells are also introduced into propulsion systems. 
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546 |a English 
650 7 |a Technology: general issues  |2 bicssc 
650 7 |a History of engineering & technology  |2 bicssc 
653 |a auto-ignition 
653 |a supersonic flow 
653 |a initial flame kernel 
653 |a oblique shock 
653 |a recirculating region 
653 |a improved body force model 
653 |a off-design 
653 |a Reynolds-averaged Navier-Stokes equations 
653 |a meridional entropy gradient 
653 |a rotor 37 
653 |a rolling motion 
653 |a subcooled flow boiling 
653 |a transverse flow 
653 |a subchannel 
653 |a VOF 
653 |a printed circuit heat exchanger 
653 |a NACA airfoil fins 
653 |a micro gas turbine recuperator 
653 |a thermo-hydraulic 
653 |a parametric study 
653 |a ventilation 
653 |a solar greenhouse 
653 |a numerical simulation 
653 |a system design 
653 |a n/a 
653 |a thrust vector control 
653 |a supersonic jet 
653 |a nozzle 
653 |a flow entrainment 
653 |a Coanda effect 
653 |a schlieren method 
653 |a scramjet 
653 |a regenerative cooling 
653 |a coupled heat transfer 
653 |a pyrolysis 
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856 4 0 |a www.oapen.org  |u https://directory.doabooks.org/handle/20.500.12854/101383  |7 0  |z DOAB: description of the publication