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 …
Hydrogen fuel in scramjet engines-a brief review
G Choubey, D Yuvarajan, W Huang, L Yan… - International Journal of …, 2020 - Elsevier
Due to the wide flammability range and low ignition delay of Hydrogen, it can burn rapidly
and generate a large amount of thrust. It is for this reason alone that many researchers have …
and generate a large amount of thrust. It is for this reason alone that many researchers have …
Supersonic mixing in airbreathing propulsion systems for hypersonic flights
W Huang, Z Du, L Yan, Z **a - Progress in Aerospace Sciences, 2019 - Elsevier
Achieving efficient fuel-air mixing is a crucial problem for the design of scramjet engines.
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …
A review of the scramjet experimental data base
The frontier in hypersonic flights via an air-breathing scramjet faces a formidable challenge,
because the operational principle is built on thermal compression, which is inherently …
because the operational principle is built on thermal compression, which is inherently …
Supersonic combustion of hydrogen using an improved strut injection scheme
Numerical investigation of mixing is performed at Mach 2.0 model Scramjet combustor
employing parallel strut injection schemes for fuel. In the present investigation, basic strut …
employing parallel strut injection schemes for fuel. In the present investigation, basic strut …
Effect of inclined fuel injection in the strut wake region for a hydrogen fueled scramjet combustor
OR Kummitha - International Journal of Hydrogen Energy, 2022 - Elsevier
The supersonic airflow and injected fuel stream mixing process is complicated for a scramjet
combustor because of little supersonic air resident time and high airflow stream momentum …
combustor because of little supersonic air resident time and high airflow stream momentum …
Numerical investigation on the performance and combustion characteristics of a cavity based scramjet combustor with novel strut injectors
SS Yarasai, D Ravi, S Yoganand… - International Journal of …, 2023 - Elsevier
A three-dimensional numerical investigation has been carried out on the performance and
combustion characteristics of a scramjet combustor with and without cavity for various strut …
combustion characteristics of a scramjet combustor with and without cavity for various strut …
Numerical investigations on the implication of hydrogen fuel jet injection pressure on the performance characteristics in a multi-strut in a double-dual cavity-based …
To analyze the influence of flow physics and operating parameters (ie, injection pressure (2,
4, 6, and 8 bars), a simulation is performed on a scramjet combustor (modified) using the …
4, 6, and 8 bars), a simulation is performed on a scramjet combustor (modified) using the …
A brief review on the recent advancement in the field of jet engine-scramjet engine
SCRAMJET engine has become one of the most recent advancement in the field of air
breathing hypersonic flight. This paper gives a brief review on recent developments of …
breathing hypersonic flight. This paper gives a brief review on recent developments of …
Optimization of scramjet performance with different fuel injection techniques and flame holder cavities
In this research paper an attempt has been made to find out the effect of passive fuel
injection and direct fuel injection along with two different cavity flame holders. In this …
injection and direct fuel injection along with two different cavity flame holders. In this …