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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Jezik:engleski
Izdano: MDPI - Multidisciplinary Digital Publishing Institute 2023
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collection Directory of Open Access Books
description 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.
format Online
id doab-20.500.12854ir-101383
institution Directory of Open Access Books
language eng
publishDate 2023
publishDateRange 2023
publishDateSort 2023
publisher MDPI - Multidisciplinary Digital Publishing Institute
publisherStr MDPI - Multidisciplinary Digital Publishing Institute
record_format ojs
spelling doab-20.500.12854ir-1013832024-04-09T23:16:09Z Advanced Propulsion System and Thermal Management Technology Liu, Jian Liu, Chaoyang Tong, Yiheng Sunden, Bengt auto-ignition supersonic flow initial flame kernel oblique shock recirculating region improved body force model off-design Reynolds-averaged Navier–Stokes equations meridional entropy gradient rotor 37 rolling motion subcooled flow boiling transverse flow subchannel VOF printed circuit heat exchanger NACA airfoil fins micro gas turbine recuperator thermo-hydraulic parametric study ventilation solar greenhouse numerical simulation system design n/a thrust vector control supersonic jet nozzle flow entrainment Coanda effect schlieren method scramjet regenerative cooling coupled heat transfer pyrolysis thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and 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 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. 2023-07-14T14:28:54Z 2023-07-14T14:28:54Z 2023 book ONIX_20230714_9783036580043_82 9783036580043 9783036580050 https://directory.doabooks.org/handle/20.500.12854/101383 eng image/jpeg Attribution 4.0 International https://mdpi.com/books/pdfview/book/7479 https://mdpi.com/books/pdfview/book/7479 MDPI - Multidisciplinary Digital Publishing Institute 10.3390/books978-3-0365-8005-0 10.3390/books978-3-0365-8005-0 46cabcaa-dd94-4bfe-87b4-55023c1b36d0 9783036580043 9783036580050 126 Basel open access
spellingShingle auto-ignition
supersonic flow
initial flame kernel
oblique shock
recirculating region
improved body force model
off-design
Reynolds-averaged Navier–Stokes equations
meridional entropy gradient
rotor 37
rolling motion
subcooled flow boiling
transverse flow
subchannel
VOF
printed circuit heat exchanger
NACA airfoil fins
micro gas turbine recuperator
thermo-hydraulic
parametric study
ventilation
solar greenhouse
numerical simulation
system design
n/a
thrust vector control
supersonic jet
nozzle
flow entrainment
Coanda effect
schlieren method
scramjet
regenerative cooling
coupled heat transfer
pyrolysis
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology
Advanced Propulsion System and Thermal Management Technology
title Advanced Propulsion System and Thermal Management Technology
title_full Advanced Propulsion System and Thermal Management Technology
title_fullStr Advanced Propulsion System and Thermal Management Technology
title_full_unstemmed Advanced Propulsion System and Thermal Management Technology
title_short Advanced Propulsion System and Thermal Management Technology
title_sort advanced propulsion system and thermal management technology
topic auto-ignition
supersonic flow
initial flame kernel
oblique shock
recirculating region
improved body force model
off-design
Reynolds-averaged Navier–Stokes equations
meridional entropy gradient
rotor 37
rolling motion
subcooled flow boiling
transverse flow
subchannel
VOF
printed circuit heat exchanger
NACA airfoil fins
micro gas turbine recuperator
thermo-hydraulic
parametric study
ventilation
solar greenhouse
numerical simulation
system design
n/a
thrust vector control
supersonic jet
nozzle
flow entrainment
Coanda effect
schlieren method
scramjet
regenerative cooling
coupled heat transfer
pyrolysis
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology
topic_facet auto-ignition
supersonic flow
initial flame kernel
oblique shock
recirculating region
improved body force model
off-design
Reynolds-averaged Navier–Stokes equations
meridional entropy gradient
rotor 37
rolling motion
subcooled flow boiling
transverse flow
subchannel
VOF
printed circuit heat exchanger
NACA airfoil fins
micro gas turbine recuperator
thermo-hydraulic
parametric study
ventilation
solar greenhouse
numerical simulation
system design
n/a
thrust vector control
supersonic jet
nozzle
flow entrainment
Coanda effect
schlieren method
scramjet
regenerative cooling
coupled heat transfer
pyrolysis
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues
thema EDItEUR::T Technology, Engineering, Agriculture, Industrial processes::TB Technology: general issues::TBX History of engineering and technology
url ONIX_20230714_9783036580043_82