Luminescence-Based Surface Measurement Technique for Simultaneous Pressure and Temperature Measurements within Non-Oxygen Based Hypersonic Ground Test Facilities
AI Overview
This RFP seeks development of a luminescence-based measurement technique to simultaneously capture pressure and temperature data in non-oxygen hypersonic wind tunnels. Current pressure-sensitive paint technology requires oxygen in the flow, limiting advanced facilities like nitrogen-based tunnels to discrete measurements.
This summary is AI-generated from the official solicitation.
Key Details
Official Description
Within aerodynamic testing, pressure sensitive paint (PSP) provides crucial global surface pressure data that is utilized in calculating aerodynamic loads [1] and identifying small scale features within the flow. The working principle behind PSP involves luminophores that fluoresce at an intensity inversely proportional to the number of oxygen molecules present i.e., oxygen quenching [2].
While these paints/luminophores have been sufficiently researched, the use-case of these paints is severely...
Change History
Luminescence-Based Surface Measurement Technique for Simultaneous Pressure and Temperature Measurements within Non-Oxygen Based Hypersonic Ground Test Facilities
New opportunity: Luminescence-Based Surface Measurement Technique for Simultaneous Pressure and Temperature Measurements within Non-Oxygen Based Hypersonic Ground Test Facilities
Similar Opportunities
Get Alerts for Opportunities Like This
RallyProp monitors thousands of funding sources and sends instant alerts when opportunities match your technology and capabilities.
Start Free Trial