Identification of a Scramjet Isolator Model from Computational Fluid Dynamics Data
Scramjet Isolator Shock-Train Leading-Edge Location Modeling
2012-2808 Detection and Transient Dynamics Modeling of Experimental Hypersonic Inlet Unstart
Acetone LIF For Flow Visualization at Temperatures Below 300 K
Heat Flux Measurements in a Scramjet Combustor Using Direct Write Technology
Closed-Loop Control of Shock Location in Mach 1.8 Direct Connect Wind Tunnel (AIAA 2014-2935)