Burst-mode planar laser-induced fluorescence of nitric oxide in the Sandia free-piston shock tunnel.
Abstract not provided.
Kearney, Sean↗
Engineering topics
Lynch, Kyle
Publications and source records attributed to Lynch, Kyle.
High Temperature Gladstone-Dale Coefficient Measurements in a Free-Piston Shock Tube.
Abstract not provided.
Wang, Gwendolyn↗
Laser Absorption Spectroscopy Measurements of High Pressure and Temperature Aluminum Combustion in a Shock Tube.
Abstract not provided.
Daniel, Kyle↗
Near-IR Laser Absorption Measurements of Atomic Nitrogen, Oxygen, and Carbon Concentrations in Shock-Heated Air.
Abstract not provided.
Jans, Elijah↗
Wall-Modeled Large-Eddy Simulation of Turbulent Mach 14 Boundary Layer for Aero-Optical Analysis.
Abstract not provided.
Castillo, Pedro↗
Nitric Oxide Emission Spectroscopy of a Cylinder Stagnation Flow in the Sandia Reflected Shock Tunnel.
Abstract not provided.
Daniel, Kyle↗
Overview of Ablation Research at Sandia National Laboratories.
Abstract not provided.
Roberts, Scott Alan↗
Towards the measurement of ablation products in hypersonic boundary layers.
Abstract not provided.
Hargis, Joshua↗
High Enthalpy Differential Equation-Based Estimates for Spherical/Cylindrical Forebody Shock Stand-off Distance .
Abstract not provided.
Dechant, Lawrence↗
High Temperature Gladstone-Dale Coefficient Measurements in a Free-Piston Shock Tube.
Abstract not provided.
Wang, Gwendolyn↗
High Enthalpy Differential Equation-Based Estimates for Spherical/Cylindrical Forebody Shock Stand-off Distance .
Abstract not provided.
Dechant, Lawrence↗
Wall-Modeled Large-Eddy Simulations of Turbulent Boundary Layer over a Flat-Plate for Aero-Optical Distortion Analysis.
Abstract not provided.
Castillo, Pedro↗
A CFD Validation Challenge for Transonic, Shock-Induced Separated Flow.
Abstract not provided.
Lance, Blake↗
Wall-Modeled Large-Eddy Simulations of Turbulent Mach 3.5, 8, and 14 Boundary Layers - Effect of Mach Number on Aero-Optical Distortions.
Abstract not provided.
Castillo, Pedro↗