[HTML][HTML] Research progress on solid-fueled Scramjet

Z Xiang, XIA Zhixun, MA Likun, LI Chaolong… - Chinese Journal of …, 2022 - Elsevier
The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet. It shows
significant advantages such as simple fuel supply and compactness, avoiding the complex …

Numerical investigation on the combustion characteristics of aluminum powder fuel in a supersonic cavity-based combustor

Y Feng, S Luo, J Song, K Xia, D Xu - Applied Thermal Engineering, 2023 - Elsevier
In order to explore the propulsion performance and combustion organization rules of powder
fueled scramjets, research on powder fuel combustion characteristics in a supersonic cavity …

Numerical investigation on regression rate and thrust regulation behaviors of a combined solid rocket motor with aluminum-based fuel

X Zou, N Wang, L Han, T Bai, K Xie - Aerospace Science and Technology, 2021 - Elsevier
The aims of this study are to determine the behaviors of regression rate and thrust regulation
of a combined solid rocket motor, which is capable of achieving energy management. A …

Optimizing combustion performance in a solid rocket scramjet engine

J Liu, N Wang, J Wang, Z Li - Aerospace Science and Technology, 2020 - Elsevier
To enhance combustion efficiency of a boron-based propellant solid rocket scramjet (SRS)
engine, this study attempted a new organization scheme combining cavity and pneumatic …

Contribution of Unsteadiness to Solid Fuel Burning Characteristics in a Scramjet Combustor

H Pace, E Schlussel, G Young, L Massa - Journal of Propulsion and …, 2024 - arc.aiaa.org
The contributions of unsteadiness to solid fuel combustion are investigated numerically and
validated against new experiments in a deep cavity scramjet. Large-eddy simulations …

Experimental investigation on the ignition delay of fuel-rich mixture in solid rocket scramjet

C Li, Z Xia, L Ma, X Zhao, B Chen, Y Feng, P Yang - Acta Astronautica, 2022 - Elsevier
In this paper, the effects of equivalence ratio and solid propellant composition on the ignition
delay time of fuel-rich mixture in solid rocket scramjets were experimentally investigated for …

Experimental study on the influence of the injection structure on solid scramjet performance

P Yang, Z Xia, L Ma, B Chen, Y Feng, J Zhang - Acta Astronautica, 2021 - Elsevier
Injection structures can affect the ignition and combustion of fuel and supersonic air in
scramjets, strongly impacting their performance. The influence of three different injection …

Experimental and numerical study of solid rocket scramjet combustor equipped with combined cavity and strut device

C Li, Z Xia, L Ma, X Zhao, B Chen - Acta Astronautica, 2019 - Elsevier
In this paper, a new solid rocket scramjet equipped with two combined cavity and strut
device was studied by experimental and numerical approaches. The experiment simulated a …

Performance evaluation for scramjet based on ground direct-connected test: A method investigation

C Li, Z Xia, L Ma, X Zhao, B Chen, P Yang - Aerospace Science and …, 2021 - Elsevier
Scramjet has become one of the most efficient hypersonic vehicles because of its broad
application potentiality. The ground direct-connected test is a relatively easy and economical …

Influence of the vortex generator on the performance of solid rocket scramjet combustor

C Li, X Zhao, Z Xia, L Ma, B Chen - Acta Astronautica, 2019 - Elsevier
In this paper, the influence of vortex generator on the performance of solid scramjet was
investigated by means of direct-connected fire tests. The experiments simulated a flight …