Implementing Pressure Sensitive Paint in the AFRL Subsonic Aerodynamic Research Laboratory
Special Probes for Measurements of Flow Parameters in a Gas-Turbine Engine
An optical technique for detecting fatigue cracks in aerospace structures
An Optical Technique for Detecting Fatigue Cracks in Aerospace Structures
Electronically scanned pressure measurement scanner for cryogenic wind tunnel applications
Electronically Scanned Pressure Measurement Scanner for Cryogenic Wind Tunnel Applications
Pressure and temperature measurements with a dual-luminophor coating
Pressure and Temperature Measurements with a Dual-Luminophor Coating
LIF Imaging of Species and Temperature in Technical Combustion at Elevated Pressures
LIF imaging of species and temperature in technical combustion at elevated pressures
Experimental Investigations on Vortex Breakdown over Delta Wings with Doppler Global Velocimetry
Application of 3 component laser-Doppler velocimetry in transonic flow over a delta wing
Application of 3 Component Laser-Doppler Velocimetry in Transonic Flow Over a Delta Wing
Development and Applications of a Rapid Flight Test Prototyping System for Unmanned Air Vehicles
Pressure Sensitive Paint Measurements on a Wing Model in a Low-Speed Wind Tunnel
Pressure-Sensitive Paint Measurements in a Large Scale Commercial Engine Test Stand
Feasibility of Airfoil Tests with a Small High Subsonic Cryogenic Wind Tunnel