Review of combustion stabilization for hypersonic airbreathing propulsion
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …
Review of cavity ignition in supersonic flows
Z Cai, T Wang, M Sun - Acta Astronautica, 2019 - Elsevier
The cavity-based flameholder is a promising device in supersonic combustion issues in a
scramjet engine and it also provides a favorable ignition environment inside the cavity owing …
scramjet engine and it also provides a favorable ignition environment inside the cavity owing …
Mechanism of a transverse jet mixing enhanced by high-frequency plasma energy deposition
H Wang, Y Yang, W Hu, G Wang, F Xie, X Fan - Physics of Fluids, 2023 - pubs.aip.org
The mixing mechanism of a transverse jet enhanced by high-frequency plasma energy
deposition is investigated at Ma= 6.13 using both experimental measurements and …
deposition is investigated at Ma= 6.13 using both experimental measurements and …
Experimental study of arc plasma energy deposition flow control on supersonic cavity combustor
A Wang, Z Chen, L Feng, H Ding, Z Huang, L Tian - Physics of Fluids, 2024 - pubs.aip.org
This investigation conducted an experimental study of flow control in a Mach 2.5 cavity
combustor using arc plasma energy deposition (APED), implemented both with and without …
combustor using arc plasma energy deposition (APED), implemented both with and without …
Effect of pulsed plasma on the scramjet combustor
To clarify the effect of pulsed plasma on the scramjet combustor and find the best area of
pulsed plasma effect in the cavity, the effects of pulsed plasma on the pressure distribution …
pulsed plasma effect in the cavity, the effects of pulsed plasma on the pressure distribution …
Scramjet Plasma Ignition and Assisted Combustion Technology Review Check for updates
The use of plasma technology to assist scramjet ignition and combustion has been a
research hotspot in the field of supersonic propulsion technology. This paper summarizes …
research hotspot in the field of supersonic propulsion technology. This paper summarizes …
Scramjet Plasma Ignition and Assisted Combustion Technology Review
The use of plasma technology to assist scramjet ignition and combustion has been a
research hotspot in the field of supersonic propulsion technology. This paper summarizes …
research hotspot in the field of supersonic propulsion technology. This paper summarizes …
Vortex Generator Based on Spark Discharge
AA Firsov, E Dolgov, SB Leonov - AIAA Scitech 2019 Forum, 2019 - arc.aiaa.org
A numerical simulation of the high-speed jet caused by the decay of the thermal cavity after
cylindrical 10 mm long spark discharge located on the surface in ambient air is performed. It …
cylindrical 10 mm long spark discharge located on the surface in ambient air is performed. It …