Mixing augmentation induced by the combination of the oblique shock wave and secondary recirculation jet in a supersonic crossflow
Published 2021 View Full Article
- Home
- Publications
- Publication Search
- Publication Details
Title
Mixing augmentation induced by the combination of the oblique shock wave and secondary recirculation jet in a supersonic crossflow
Authors
Keywords
Shock wave/jet shear layer interaction, Hydrogen, Secondary recirculation jet, Mixing efficiency, Separation zone, Recirculation zone
Journal
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
Volume 47, Issue 11, Pages 7458-7477
Publisher
Elsevier BV
Online
2021-12-26
DOI
10.1016/j.ijhydene.2021.12.069
References
Ask authors/readers for more resources
Related references
Note: Only part of the references are listed.- Effect of a revolved wedge strut induced mixing enhancement for a hydrogen fueled scramjet combustor
- (2021) Obula Reddy Kummitha et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Design exploration on the shock wave/turbulence boundary layer control induced by the secondary recirculation jet
- (2021) Zhao-bo Du et al. ACTA ASTRONAUTICA
- Effects of cavity-induced mixing enhancement under oblique shock wave interference: Numerical study
- (2021) Zuo Qiuru et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Numerical investigation on mixing improvement mechanism of transverse injection based scramjet combustor
- (2021) Gautam Choubey et al. ACTA ASTRONAUTICA
- Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine
- (2021) Dai Jian et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Hydrogen fueled scramjet combustor with a wavy-wall double strut fuel injector
- (2021) Obula Reddy Kummitha et al. FUEL
- The influence of the wedge shock generator on the vortex structure within the trapezoidal cavity at supersonic flow
- (2020) Zhixiong Li et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Numerical investigation of upstream cavity enhanced fuel mixing in scramjet combustors
- (2020) Tim Roos et al. ACTA ASTRONAUTICA
- Shock wave/turbulence boundary layer interaction control with the secondary recirculation jet in a supersonic flow
- (2020) Li Yan et al. ACTA ASTRONAUTICA
- Numerical simulations of high frequency transverse pulsed jet injection into a supersonic crossflow
- (2020) Nehemiah J. Williams et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows
- (2020) Wei Huang et al. ACTA ASTRONAUTICA
- Flame stabilization enhancement in a strut-based supersonic combustor by shock wave generators
- (2020) Bin An et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Wall temperature effects on shock wave/turbulent boundary layer interaction via direct numerical simulation
- (2020) Ke Zhu et al. ACTA ASTRONAUTICA
- Effect of wavy wall strut fuel injector on shock wave development and mixing enhancement of fuel and air for a scramjet combustor
- (2020) Obula Reddy Kummitha et al. Journal of Computational Design and Engineering
- Supersonic mixing in airbreathing propulsion systems for hypersonic flights
- (2019) Wei Huang et al. PROGRESS IN AEROSPACE SCIENCES
- RANS study of steady and pulsed gaseous jets into a supersonic crossflow
- (2019) Zhao-bo Du et al. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER
- URANS study of pulsed hydrogen jet characteristics and mixing enhancement in supersonic crossflow
- (2019) Majie Zhao et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Numerical study of flow structures and mixing characteristics of a sonic jet in supersonic crossflow
- (2019) Chang-hai Liang et al. ACTA ASTRONAUTICA
- The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow
- (2019) Yicheng Li et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Characteristics of laser ignition and spark discharge ignition in a cavity-based supersonic combustor
- (2019) Bin An et al. COMBUSTION AND FLAME
- The effect of sinusoidal wall on hydrogen jet mixing rate considering supersonic flow
- (2019) Zhixiong Li et al. ENERGY
- Numerical simulation of mixing of hydrogen jet at supersonic cross flow in presence of upstream wavy wall
- (2019) Tran Dinh Manh et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Shock wave structures in the wake of sonic transverse jet into a supersonic crossflow
- (2018) Chang-hai Liang et al. ACTA ASTRONAUTICA
- Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight
- (2018) Javier Urzay Annual Review of Fluid Mechanics
- Mixing improvement induced by the combination of a micro-ramp with an air porthole in the transverse gaseous injection flow field
- (2018) Lang-quan Li et al. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER
- Numerical analysis of hydrogen fueled scramjet combustor with innovative designs of strut injector
- (2018) Obula Reddy Kummitha et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Mixing augmentation mechanism induced by the dual injection concept in shcramjet engines
- (2018) Zhao-bo Du et al. ACTA ASTRONAUTICA
- Effect of flow distortion on fuel/air mixing and combustion in an upstream-fueled cavity flameholder for a supersonic combustor
- (2017) Steven Etheridge et al. EXPERIMENTAL THERMAL AND FLUID SCIENCE
- Effects of micro-ramp on transverse jet in supersonic crossflow
- (2016) Yujie Zhang et al. ACTA ASTRONAUTICA
- Investigation on supersonic combustion of hydrogen with variation of combustor inlet conditions
- (2016) Vishnu Hariharan et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Study of sonic injection from circular injector into a supersonic cross-flow using large eddy simulation
- (2016) Majie Zhao et al. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
- Fluidic Control Method for Improving the Self-Starting Ability of Hypersonic Inlets
- (2016) Jian-Yong Wang et al. JOURNAL OF PROPULSION AND POWER
- Effects of Incident Shockwave on Flame-holding Downstream of Ramp Injector in Supersonic Flow
- (2016) Yoshitaka IWAMURA et al. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
- Mixing augmentation induced by the interaction between the oblique shock wave and a sonic hydrogen jet in supersonic flows
- (2015) Wei Huang et al. ACTA ASTRONAUTICA
- Numerical study of oblique shock-wave/boundary-layer interaction considering sidewall effects
- (2015) Bo Wang et al. JOURNAL OF FLUID MECHANICS
- Large-eddy simulation of passive shock-wave/boundary-layer interaction control
- (2014) Vito Pasquariello et al. INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW
- Numerical prediction on the interaction between the incident shock wave and the transverse slot injection in supersonic flows
- (2012) Wei Huang et al. AEROSPACE SCIENCE AND TECHNOLOGY
- Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows
- (2011) Wei Huang et al. ACTA ASTRONAUTICA
Publish scientific posters with Peeref
Peeref publishes scientific posters from all research disciplines. Our Diamond Open Access policy means free access to content and no publication fees for authors.
Learn MoreAsk a Question. Answer a Question.
Quickly pose questions to the entire community. Debate answers and get clarity on the most important issues facing researchers.
Get Started