Using internal air injection for fuel mixing enhancement of annular hydrogen jet behind an inclined strut in a supersonic combustor: computational study. [PDF]
Bouazzi Y +7 more
europepmc +1 more source
Mach 10 Computational Study of a Three-Dimensional Scramjet Inlet Flow Field
The present work documents the computational results for a combined computational and experimental parametric study of the internal aerodynamics of a generic three-dimensional sidewall-compression scramjet inlet configuration at Mach 10.
Scott D. Holland
core
A Wavelength Modulation Spectroscopy-Based Methane Flux Sensor for Quantification of Venting Sources at Oil and Gas Sites. [PDF]
Festa-Bianchet SA +3 more
europepmc +1 more source
Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study. [PDF]
Mir A +7 more
europepmc +1 more source
High fidelity simulations of unstart phenomena in a scramjet inlet due to angle of attack [PDF]
This work investigates the unsteady behavior of unstart phenomena within a scramjet inlet using advanced computational techniques. Scramjets and ramjets, with their reliance on inlet compression, offer promising airbreathing propulsion for hypersonic ...
Bravo, Luis +4 more
core
Numerical simulation of ellipse liquid jet atomization in supersonic crossflow. [PDF]
Zhou D, Li Y, Chang J.
europepmc +1 more source
Effects of Hydrogen Multijet and Flow Rate Assignment on the Combustion Flow Characteristics in a Jet-Stabilized Combustor. [PDF]
Sun H +5 more
europepmc +1 more source
Effect of Kerosene Dual-Jet Spacing on the Mixing and Combustion Characteristics of a Scramjet Combustor. [PDF]
Peng SS +5 more
europepmc +1 more source
Explore artificial neural networks for solving complex hydrocarbon chemistry in turbulent reactive flows. [PDF]
An J, Qin F, Zhang J, Ren Z.
europepmc +1 more source
Evaluation of Influences of Changed Lower Cover Geometry on Kerosene-Air Interaction in a Scramjet Combustor. [PDF]
Peng SS, Zhou WX, Shi HH, Li RW, Zhu L.
europepmc +1 more source

