Rationale for Ground Test Development of Scramjet Inlets
Rationale for Ground Test Development of Scramjet Inlets
Internal Flowfield Characteristics of a Two-Dimensional Scramjet Inlet at Mach 10
Internal Flowfield Characteristics of a Two-Dimensional Scramjet Inlet at Mach 10
Energy Based Framework for Assessment of Energetic Flow Control Techniques (Invited) AIAA Paper
Energy Based Plasma Performance Specifications for Flight Vehicles
Generalized Energetic Efficiency Metrics for Flight Vehicle System Evaluation
Surface Microwave Discharge in Quasi-Optical Wave Beam AIAA Paper
Microwave Discharge in Quasi-optical Wave Beam AIAA Paper
Magnetohydrodynamic Influence on a Supersonic Nitrogen Flow About a Body of Revolution AIAA Paper
Investigation of Magnetohydrodynamic Interaction in a Supersonic Flow about a Body of Revolution
Deeply Subcritical MW Discharge in the Submerged Stream of Propane-Air Mixture
IMPACT OF A MAGNETIC FIELD ON ROTATION OF A GAS DISCHARGE AROUND AN AXISYMMETRIC BODY
RESEARCH ISSUES RESULTING FROM AN ASSESSMENT OF TECHNOLOGIES FOR FUTURE HYPERSONIC AEROSPACE SYSTEMS
Control of a Supersonic Nitrogen Flow by a Magnetic Field
Thermal Measurements at the Body Surface in a Supersonic Nitrogen Flow AIAA Paper
CHARACTERIZATION OF SPARKJET ACTUATORS FOR FLOW CONTROL
MHD POWER GENERATION IN SCRAMJET ENGINES IN CONJUNCTION WITH INLET CONTROL
MHD CONTROL OF THE SEPARATION PHENOMENON IN A SUPERSONIC XENON PLASMA FLOW. II