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 …
Supersonic combustion in air-breathing propulsion systems for hypersonic flight
J Urzay - Annual Review of Fluid Mechanics, 2018 - annualreviews.org
Great efforts have been dedicated during the last decades to the research and development
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
of hypersonic aircrafts that can fly at several times the speed of sound. These aerospace …
Supersonic spray combustion subject to scramjets: Progress and challenges
Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …
occurs in the scramjet propulsion system, and related research can motivate the …
Large eddy simulation of turbulent supersonic hydrogen flames with OpenFOAM
A high-fidelity numerical solver, RYrhoCentralFoam, is developed based on OpenFOAM® to
simulate turbulent compressible reactive flows. It is designed for accurately simulating …
simulate turbulent compressible reactive flows. It is designed for accurately simulating …
Lift-off behaviors of the partially-premixed jet flame in a supersonic vitiated coflow
C Liu, J Zhang, X Li, Y Pan, W Huang - Aerospace Science and …, 2023 - Elsevier
Achieving fast and efficient combustion is considered as the primary difficulty in overcoming
the high-Mach-number scramjet. A novel injection strategy with coflows has been proposed …
the high-Mach-number scramjet. A novel injection strategy with coflows has been proposed …
Ignition and flame stabilization characteristics in an ethylene-fueled scramjet combustor
C Liu, M Sun, H Wang, L Yang, B An, Y Pan - Aerospace Science and …, 2020 - Elsevier
Successful ignition process is the prerequisite for achieving stable combustion in a scramjet
combustor coupled with a cavity. A single pulse laser is adopted to ignite the fuel/air mixture …
combustor coupled with a cavity. A single pulse laser is adopted to ignite the fuel/air mixture …
Nonlinear multispectral tomographic absorption deflection spectroscopy based on Bayesian estimation for spatially resolved multiparameter measurement in methane …
Z Niu, H Qi, Z Zhu, Y Ren, M He, B Gao - Fuel, 2024 - Elsevier
In aerospace propulsion systems with high temperature, pressure, and distortion,
inhomogeneous thermophysical gradients can cause line-of-sight deflection and spectral …
inhomogeneous thermophysical gradients can cause line-of-sight deflection and spectral …
Numerical investigation of low-frequency instability and frequency shifting in a scramjet combustor
The combustion instability in a laboratory-scale direct-connect hydrogen-fueled scramjet
combustor is investigated numerically. The numerical simulation has been carried out using …
combustor is investigated numerically. The numerical simulation has been carried out using …
Analysis of combustion modes in a cavity based scramjet
Large eddy simulations (LES) of non reactive and reactive flows in a cavity-based scramjet
combustor configuration from the US Air Force Research Laboratory (AFRL) are performed …
combustor configuration from the US Air Force Research Laboratory (AFRL) are performed …
Mid-infrared laser absorption tomography for quantitative 2D thermochemistry measurements in premixed jet flames
A tomographic laser absorption spectroscopy technique, utilizing mid-infrared light sources,
is presented as a quantitative method to spatially resolve species and temperature profiles …
is presented as a quantitative method to spatially resolve species and temperature profiles …