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Advanced Propulsion System and Thermal Management Technology
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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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Keywords
- auto-ignition
- coanda effect
- coupled heat transfer
- flow entrainment
- History of engineering & technology
- improved body force model
- initial flame kernel
- meridional entropy gradient
- micro gas turbine recuperator
- n/a
- NACA airfoil fins
- nozzle
- Numerical Simulation
- oblique shock
- off-design
- parametric study
- printed circuit heat exchanger
- pyrolysis
- recirculating region
- regenerative cooling
- Reynolds-averaged Navier–Stokes equations
- rolling motion
- rotor 37
- schlieren method
- scramjet
- solar greenhouse
- subchannel
- subcooled flow boiling
- supersonic flow
- supersonic jet
- System design
- Technology, engineering, agriculture
- Technology: general issues
- thermo-hydraulic
- thrust vector control
- transverse flow
- Ventilation
- VOF
Links
DOI: 10.3390/books978-3-0365-8005-0Editions