Discover Supersonic Combustion

Effect of density gradients in confined supersonic shear layers

Laser-initiated conical detonation wave for supersonic combustion

Heat release effects on mixing in supersonic reacting free shear-layers

Supersonic combustion of hydrogen injected perpendicular to a ducted vitiated airstream

A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustor

A review of supersonic combustion research at AEDC with hypersonic applications

Instrumentation development for study of Reynolds analogy in reacting flows

Evaluation of parallel injector configurations for supersonic combustion

A comparative study of scramjet injection strategies for high Mach number flows

A numerical study of mixing enhancement in a supersonic combustor

Mixing and combustion enhancement from unsteady shock-fuel layer interactions

Navier-Stokes simulation of the supersonic combustion flowfield in a ram accelerator

Analysis of losses in supersonic mixing and reacting flows

Mixing enhancement in a supersonic combustor

An analytical and computational investigation of shock-induced vortical flows with applications to supersonic combustion

Planar Rayleigh scattering and laser-induced fluorescence for visualization of a hot, Mach 2 annular air jet

Effect of heat release on the spatial stability of a supersonic reacting mixing layer

Vorticity generation by contoured wall injectors

A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection

Preliminary calibration of a generic scramjet combustor

Diagnostics in supersonic combustion

The aerospace plane design challenge

Fuel-rich catalytic combustion of a high density fuel

Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program