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
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
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
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
Doppler Global Velocimetry: accuracy tests in a wind tunnel
Pressure Sensitive Paint for Oscillating Pressure Fields Measurements
Measurement Technology of the Impact of Alumina Liquid Particles on a Hot Surface
A Comparative Study of Planar Mie and Rayleigh Scattering for Supersonic Flowfield Diagnostics
Flow Velocity Visualization Using Doppler Picture Interference Velocimetry
Investigations on a Dynamic Forebody Flow Control System
The Recent Methods for Surface Pressure and Skin Friction Measurements on the Models
Phosphor Thermography for High Temperature Gas Turbine Applications
Multiple Point Dynamic Gas Density Measurements Using Molecular Rayleigh Scattering
Fuzzy Logic Enhanced Digital PIV Processing Software
A Re-Evaluation of a Pulsed Laser Technique for Measuring Surface Heat Transfer Co-Efficients
LDA System for In-Flight Local Velocity Measurements on Airplane Wings
Performance Studies of the Constant Voltage Anemometer in a Mach 2.3 Boundary Layer
3-Component-Doppler-Laser-2-Focus: a New Kind of Three Component Velocimeter
Quantitative Flow Field Measurements in a Catapult Facility Using Particle Image Velocimetry
Non-Intrusive Diagnostics for the AEDC Impulse Facility: Applications and Results
Incompressible Aerodynamics of a Planetary Entry Capsule
Vortical Flow Field Investigation Using a Two-Component Pressure Sensitive Paint at Low Speed
Comparison of Luminescent Paints Measurement Systems
Status of Pressure-Sensitive Paint Technology at NAL
Laser Anemometer Measurements in a Centrifugal Compressor
Particle Image Velocimetry to quantify 3D-Flow Properties of Gas Turbine Forced Mixers