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title: 22nd aiaa aerospace sciences meeting and exhibit
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title: 42nd aiaa aerospace sciences meetings and exhibit
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title: 32nd aiaa aerospace sciences meeting and exhibit
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title: 42nd AIAA Aerospace Sciences Meeting and Exhibit
Observation of MHD Effects with Non-Equlibrium Ionization in Cold Supersonic Air Flows
MHD Power Generation in Scramjet Engines in Conjunction with Inlet Control
Bulk Viscosity Measurements Using Coherent Rayleigh-Brillouin Scattering
Results of the 1 MW Radiatively-Driven Hypersonic Wind Tunnel Experiments
Design and Development of a Pulsed, Narrow Linewidth UV Source for Flow Dianostics
DBD Plasma Actuators Driven by a Combination of Low Frequency Bias Voltage and Nanosecond Pulses
Diagnostics of Short Pulsed Sustained Plasmas in a Cold Air MHD Channel
Unsteady Numerical Simulation of the 1 MW Radiatively-Driven Hypersonic Wind Tunnel Experiment
Modeling of Interaction Between Weakly Ionized Near-Surface Plasmas and Gas Flow
Pulsed Microwave Enhancement of Laminar and Turbulent Hydrocarbon Flames
Optimization of Dielectric Barrier Discharge Plasma Actuators Driven By Repetitive Nanosecond Pulses
Design and Test of a Morphing Supersonic Nozzle
Ionization in Strong Electric Fields and Dynamics of Nanosecond-Pulse Plasmas
Snowplow Surface Discharge in Magnetic Field for High Speed Boundary Layer Control
Magnetically Driven Surface Discharges for Shock-Wave Induced Boundary-Layer Separation Control
Numerical Study of Shockwave Induced Boundary Layer Separation Control using Plasma Actuators
Shockwave Induced Turbulent Boundary Layer Separation Control with Plasma Actuators
Plasma-Enhanced, Hypersonic Performance Enabled by MHD Power Extraction