Sensors are perhaps the most important and integral components of our modern society.
With global warming and environmental pollution garnering ever-increasing attention, as …

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 …

The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

Kerosene distribution before its ignition in a scramjet combustor with dual cavity was
measured using kerosene-PLIF under transverse injection upstream of the cavity and …

Ignition processes in scramjet pilot cavities are highly transient events that are influenced by
factors including freestream Mach number and inlet geometry, turbulence intensity, cavity …

This work examined combustion modes in a fundamental, axisymmetric, supersonic
combustor at flight equivalent Mach numbers ranging from 7.5 to 9.0. Ethylene was injected …

With the tendency of high-speed flight and economic cruise, combustion mode in a scramjet
engine will transfer from diffusion combustion mode to premixed combustion mode because …

Hypersonic airbreathing engines rely on scramjet combustion processes, which involve high-
speed, compressible, and highly turbulent reacting flows. The combustion environment and …

Mixed conducting perovskite membrane has been intensively investigated as a possible
new technology for oxygen production to replace the conventional cryogenic distillation …

The mixing process between the injectant and air is very crucial for the engineering
implementation of the scramjet engine, and this is due to the very short resident time of fuel …