Flow Features of Dual-hole Injection in Supersonic Flow
Characteristics of Supersonic Combustion with Hartmann-Sprenger Tube Aided Fuel Injection
AIAA-2007-1133 INVESTIGATION OF MODEL SCRAMJET PERFORMANCE
Nonscan spatial heterodyne holographic spectroscopy [3559-07]
Performance of the Fuel Injector in Supersonic Combustor
Flow-Field of the Excited Jet and Mixing in a Supersonic Cross Flow