Acoustic source for compressible flow receptivity experiments
Acoustic Source for Compressible Flow Receptivity Experiments
Aerothermodynamic Issues for HIFiRE -1 Flight Vehicle
Aerothermodynamic Testing and Boundary Layer Trip Sizing of the HIFiRE Flight 1 Vehicle
Aerothermodynamic Testing and Boundary-Layer Trip Sizing of the HIFiRE Flight 1 Vehicle
AIAA 2006-0710 Surface Discharges for High-Speed Boundary Layer Control
AIAA 2006-0764 Hypersonic Inlet with Plasma Induced Compression
AIAA 2006-1172 Study of Plasma Electrode Arrangements for Optimum Lift in a Mach 5 Flow
Analyzing and Synthesizing Images by Evolving Curves with the Osher-Sethian Method
Application of Plasma Discharge Arrays to High-Speed Flow Control
Aspects of Hypersonic Boundary-Layer Transition Control
Cortex segmentation - a fast variational geometric approach
Cortex Segmentation-A Fast Variational Geometric Approach