Add to ORKGA simultaneous luminescence pressure and temperature mapping system is developed including improved dye application techniques for surface temperature and pressure measurements from 5 torr to 1000 torr with possible upgrade to from 0.5 torr to several atmospheres with improved camera resolution. Adsorbed perylene dye on slip-cast silica is pressure (oxygen) sensitive and reusable to relatively high temperatures (approximately 150 C). Adsorbed luminescence has an approximately linear color shift with temperature, which can be used for independent temperature mapping and brightness pressure calibration with temperature
Under a NASA Dryden-sponsored contract in the mid 1960s, temperatures of up to 2200 C were successfu...
A near infrared differential absorption lidar technique is developed using atmospheric oxygen as a t...
Acquiring pressure maps of aerodynamic surfaces is very important for improving and validating the p...
Pressure sensitive luminescent paints (PSP) have recently emerged as a viable technique for aerodyna...
Thermal imaging techniques are introduced using a chromatic image analysis system and temperature se...
This thesis describes various methods for time-resolved luminescence lifetime determination, and the...
Use of luminescent paints for the measurement of global pressures on wind tunnel model surfaces requ...
NASA ARC has conducted flight tests of a new type of aerodynamic pressure sensor based on a luminesc...
The luminescent paint measurement technique utilizes a coating that is applied to a test article, al...
In recent times, certain luminescent coatings, more popularly known as pressure sensitive paints (PS...
This invention relates to a noncontact imagine pyrometer system for obtaining the true temperature i...
The use of phosphor thermography for noncontact temperature measurements in harsh environments has b...
New facilities and test techniques afford research aerodynamicists many opportunities to investigate...
The overall goal of the Aeronautics Research Mission Directorate (ARMD) Seedling Phase II effort was...
Luminescent coating measurement system is a relatively new technology for quantitative pressure and ...
Under a NASA Dryden-sponsored contract in the mid 1960s, temperatures of up to 2200 C were successfu...
A near infrared differential absorption lidar technique is developed using atmospheric oxygen as a t...
Acquiring pressure maps of aerodynamic surfaces is very important for improving and validating the p...
Pressure sensitive luminescent paints (PSP) have recently emerged as a viable technique for aerodyna...
Thermal imaging techniques are introduced using a chromatic image analysis system and temperature se...
This thesis describes various methods for time-resolved luminescence lifetime determination, and the...
Use of luminescent paints for the measurement of global pressures on wind tunnel model surfaces requ...
NASA ARC has conducted flight tests of a new type of aerodynamic pressure sensor based on a luminesc...
The luminescent paint measurement technique utilizes a coating that is applied to a test article, al...
In recent times, certain luminescent coatings, more popularly known as pressure sensitive paints (PS...
This invention relates to a noncontact imagine pyrometer system for obtaining the true temperature i...
The use of phosphor thermography for noncontact temperature measurements in harsh environments has b...
New facilities and test techniques afford research aerodynamicists many opportunities to investigate...
The overall goal of the Aeronautics Research Mission Directorate (ARMD) Seedling Phase II effort was...
Luminescent coating measurement system is a relatively new technology for quantitative pressure and ...
Under a NASA Dryden-sponsored contract in the mid 1960s, temperatures of up to 2200 C were successfu...
A near infrared differential absorption lidar technique is developed using atmospheric oxygen as a t...
Acquiring pressure maps of aerodynamic surfaces is very important for improving and validating the p...