Recent research progress on transverse injection technique for scramjet applications-a brief review

G Choubey, D Yuvarajan, W Huang, A Shafee… - International Journal of …, 2020 - Elsevier
With the advancement of the air-breathing propulsion system, the supersonic vehicle
technique has drawn a significant interest worldwide. The mixing and combustion process in …

Supersonic mixing in airbreathing propulsion systems for hypersonic flights

W Huang, Z Du, L Yan, Z Xia - 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 …

Transverse jet in supersonic crossflows

W Huang - Aerospace Science and Technology, 2016 - Elsevier
The mixing and combustion process plays an important role in the realization of the scramjet
engine, and the transverse injection from a wall orifice is widely employed for the simplest …

Supersonic spray combustion subject to scramjets: Progress and challenges

Z Ren, B Wang, G Xiang, D Zhao, L Zheng - Progress in Aerospace …, 2019 - Elsevier
Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

Numerical study of shock wave interaction on transverse jets through multiport injector arrays in supersonic crossflow

MB Gerdroodbary, DD Ganji, Y Amini - Acta astronautica, 2015 - Elsevier
In the present paper, the influence of shock wave position on sonic transverse hydrogen
micro-jets in supersonic crossflow is investigated. This study focuses on mixing and shock …

Mixing augmentation induced by the interaction between the oblique shock wave and a sonic hydrogen jet in supersonic flows

W Huang, J Tan, J Liu, L Yan - Acta Astronautica, 2015 - Elsevier
The mixing process between the injectant and air is very important for the operation of
scramjet engine, and the injectant and air should be mixed sufficiently before entering into …

A methodology for estimating hypersonic engine performance by coupling supersonic reactive flow simulations with machine learning techniques

AC Ispir, BH Saracoglu, T Magin… - Aerospace Science and …, 2023 - Elsevier
We propose a methodology used to estimate the performance of hypersonic engines by
coupling some machine learning methods with a generated CFD database and one …

Large eddy simulation of flame structure and combustion mode in a hydrogen fueled supersonic combustor

Z Huang, G He, F Qin, X Wei - international journal of hydrogen energy, 2015 - Elsevier
Abstract In this study, Large Eddy Simulation (LES) of supersonic turbulent mixing and
combustion adopting a Partially Stirred Reactor (PaSR) sub-grid combustion model is …

Influence of the angle of incident shock wave on mixing of transverse hydrogen micro-jets in supersonic crossflow

MB Gerdroodbary, O Jahanian, M Mokhtari - International Journal of …, 2015 - Elsevier
A three-dimensional numerical study has been performed to investigate the influence of
angle of shock waves on sonic transverse Hydrogen micro-jets subjected to a supersonic …

A review of parametric approaches specific to aerodynamic design process

T Zhang, Z Wang, W Huang, L Yan - Acta Astronautica, 2018 - Elsevier
Parametric modeling of aircrafts plays a crucial role in the aerodynamic design process.
Effective parametric approaches have large design space with a few variables. Parametric …