Supersonic combustion in air-breathing propulsion systems for hypersonic flight
J Urzay - Annual Review of Fluid Mechanics, 2018 - annualreviews.org
Great efforts have been dedicated during the last decades to the research and development
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
[HTML][HTML] Recent research progress on airbreathing aero-engine control algorithm
Airbreathing aero-engines are regarded as excellent propulsion devices from ground takeoff
to hypersonic flight, and require control systems to ensure their efficient and safe operation …
to hypersonic flight, and require control systems to ensure their efficient and safe operation …
Survey on the mode transition technique in combined cycle propulsion systems
W Huang, L Yan, J Tan - Aerospace Science and Technology, 2014 - Elsevier
With the maturation of the scramjet technologies, the urgent development of the combined
cycle propulsion system has been put forward, and it can help the vehicle to launch and land …
cycle propulsion system has been put forward, and it can help the vehicle to launch and land …
Performance analysis and dynamic optimization of integrated cooling and power generation system based on supercritical CO2 cycle for turbine-based combined …
Turbine-based combined cycle (TBCC) engines are the most promising propulsion systems
for the horizontal takeoff and landing of hypersonic vehicles. However, the high air-inlet …
for the horizontal takeoff and landing of hypersonic vehicles. However, the high air-inlet …
Modeling and performance analysis of a pre-cooling and power generation system based on the supercritical CO2 Brayton cycle on turbine-based combined cycle …
Turbine-based combined cycle (TBCC) engines are a promising system of hypersonic
vehicles, the main problem being the thrust gap during propulsion. To solve this problem, we …
vehicles, the main problem being the thrust gap during propulsion. To solve this problem, we …
Review on the aerodynamic issues of the exhaust system for scramjet and turbine based combined cycle engine
Z Lv, J Xu, G Song, R Li, J Ge - Progress in Aerospace Sciences, 2023 - Elsevier
A review of research progress in the design of the exhaust system for the scramjet and
turbine based combined cycle (TBCC) engine is presented. Firstly, the technical challenges …
turbine based combined cycle (TBCC) engine is presented. Firstly, the technical challenges …
How close is a hydrogen hypersonic commercial aircraft?
A Boretti - International Journal of Hydrogen Energy, 2023 - Elsevier
There is a growing interest in hydrogen hypersonic commercial aircraft, which is claimed
could permit travel from Sydney to London in less than 1½ hours with reduced …
could permit travel from Sydney to London in less than 1½ hours with reduced …
Thermodynamic performance analysis of the rotating detonative airbreathing combined cycle engine
Z Ji, H Zhang, B Wang - Aerospace Science and Technology, 2021 - Elsevier
A configuration is presented for the rotating detonative airbreathing combined cycle engine
with compatibility between the turbomachinery and rotating detonation combustor being …
with compatibility between the turbomachinery and rotating detonation combustor being …
Large-eddy/Reynolds-averaged Navier–Stokes simulations of reactive flow in dual-mode scramjet combustor
JA Fulton, JR Edwards, HA Hassan… - Journal of Propulsion …, 2014 - arc.aiaa.org
Numerical simulations of the turbulent reactive flow within a model scramjet combustor
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
Development of a premixed combustion capability for dual-mode scramjet experiments
Hypersonic airbreathing engines rely on scramjet combustion processes, which involve high-
speed, compressible, and highly turbulent reacting flows. The combustion environment and …
speed, compressible, and highly turbulent reacting flows. The combustion environment and …