The development and initial demonstration of a scanned-wavelength, first-harmonic-
normalized, wavelength-modulation spectroscopy with nf detection (scanned-WMS-nf/1f) …

The facilitation of a stable combustion process is of utmost importance for the realizability
and performance of hypersonic propulsion systems. To elucidate the turbulent combustion …

The enhanced mixing and combustion mechanism of pulsed sonic jet with optimal frequency
in supersonic crossflow with a 10° ramp has been investigated using Large Eddy Simulation …

Large eddy simulation (LES) has been performed to investigate transverse hydrogen jet
mixing and combustion process in a scramjet combustor model with a compression ramp at …

Large-eddy simulations have been performed to investigate the flow coherent structures and
mixing characteristics in a Scramjet combustor having a sonic hydrogen injection from …

In this paper, we try to look into the future to envision how large eddy and detached eddy
simulations will be used in the engineering design process about 20–30 years from now …

Flame stabilization mechanisms of a hydrogen-fueled laboratory model scramjet combustor
are numerically studied. The combustor consists of a sonic fuel jet injected paralleling into a …

Since the introduction of linear array focused laser differential interferometry (LA-FLDI), its
use has rapidly proliferated as it extends the capabilities of FLDI to multiple measurement …

Characterization of the thermal gradients within supersonic and hypersonic flows is
essential for understanding transition, turbulence, and aerodynamic heating. Developments …

A turbulent combustion modeling method combining the improved delayed detached eddy
simulation (IDDES) model and the flamelet/progress variable (FPV) model is developed and …