Review of combustion stabilization for hypersonic airbreathing propulsion

Q Liu, D Baccarella, T Lee - Progress in Aerospace Sciences, 2020 - Elsevier
A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

Flame propagation and stabilization in dual-mode scramjet combustors: a survey

W Huang, Z Du, L Yan, R Moradi - Progress in Aerospace Sciences, 2018 - Elsevier
The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

Review of cavity-stabilized combustion for scramjet applications

Z Wang, H Wang, M Sun - Proceedings of the Institution of …, 2014 - journals.sagepub.com
Cavities are widely used as flameholders in supersonic combustors due to their outstanding
potential to stabilize combustion without excessive total pressure loss. A review of cavity …

Investigation of combustion process of a kerosene fueled combustor with air throttling

Y Tian, S Yang, J Le, F Zhong, X Tian - Combustion and Flame, 2017 - Elsevier
An experimental and numerical study was carried out to investigate the combustion process
of a kerosene fueled combustor with air throttling. The results were obtained with the inflow …

An experimental and kinetic study the effect of nitrogen dioxide addition on autoignition of n-heptane

L Shi, D Chen, Z Zheng, P Xu, R Wang, C Zhang - Combustion and Flame, 2021 - Elsevier
Vitiation effect is vital in the combustion-heated wind-tunnel experiments. NO 2 is an active
vitiated species which can affect the combustion properties of hydrocarbons. Ignition delay …

Dual-mode scramjet flameholding operability measurements

JM Donohue - Journal of Propulsion and Power, 2014 - arc.aiaa.org
Measurements were made in a direct-connect combustor facility designed to simulate cavity
flameholding in a hydrocarbon-fueled dual-mode scramjet combustor where the presence of …

Development of a premixed combustion capability for dual-mode scramjet experiments

RD Rockwell, CP Goyne, H Chelliah… - Journal of Propulsion …, 2018 - arc.aiaa.org
Hypersonic airbreathing engines rely on scramjet combustion processes, which involve high-
speed, compressible, and highly turbulent reacting flows. The combustion environment and …

Ethylene flame dynamics and inlet unstart in a model scramjet

Q Liu, A Passaro, D Baccarella, H Do - Journal of Propulsion and Power, 2014 - arc.aiaa.org
Ethylene flame dynamics in a model scramjet installed in an open test section of an arc-
heated hypersonic wind tunnel are experimentally investigated with freestreams of Mach 4.5 …

Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow

T Ukai, H Zare-Behtash, KH Lo, K Kontis… - International journal of …, 2014 - Elsevier
A rectangular open cavity with upstream dual injectors at a freestream Mach number of 1.9
was investigated experimentally. To evaluate the effect of the distance between the jets, the …

Experimental and numerical investigation of vitiation effects on the auto-ignition of n-heptane at high temperatures

D Zhang, Y Wang, C Zhang, P Li, X Li - Energy, 2019 - Elsevier
The ground test in wind-tunnel with high temperatures plays an important role in the
scramjet design and refinement. To simulate supersonic flight conditions, combustion …