Z Wang, H Wang, M Sun - Proceedings of the Institution of …, 2014 - journals.sagepub.com
Cavities are widely used as flameholders in supersonic combustors due to their outstanding potential to stabilize combustion without excessive total pressure loss. A review of cavity …
H Wang, X Song, L Li, Y Huang, M Sun - Aerospace Science and …, 2021 - Elsevier
Experiments are performed to investigate the near blowoff characteristics of cavity-stabilized flames in an ethylene-fueled scramjet combustor. Heated air enters the combustor with …
This work reports the experimental demonstration of single-shot visualization of turbulent flows in all three spatial dimensions (3D) based on volumetric laser induced fluorescence …
Combustion of ethylene was examined experimentally via semi-freejet testing of a fundamental, axisymmetric combustor model at conditions representative of Mach 7–8 flight …
D Baccarella, Q Liu, A Passaro, T Lee… - … Science and Technology, 2016 - iopscience.iop.org
A new pulsed-arc-heated hypersonic wind tunnel facility, designated as ACT-1 (Arc-heated Combustion Test-rig 1), has been developed and built at the University of Notre Dame in …
The dynamics of using a pulse detonation wave to ignite a supersonic cavity flameholder was investigated. Fueling conditions ranging from lean to rich were investigated …
The goal of this work was to contrast and compare the 2D and 3D flame topography of a turbulent flame. The 2D measurements were obtained using CH-based (methylidyne radical …