Heat-Flux Measurements with Temperature-Sensitive Paint in a Mach-6 Quiet Tunnel
Fluorescence control through quantum interference mechanisms in a coupled cavity waveguide
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Global Luminescent Oil-Film Skin-Friction Meter
AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Avian Wing Geometry and Kinematics
INTERDISCIPLINARY TOPICS - In Situ Calibration Uncertainty of Pressure-Sensitive Paint (TN)
TECHNICAL NOTES - Transonic Rotor Blade Pressure Measurement Using Fluorescent Paints