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Development of advanced high-temperature heat flux sensors
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Atkinson, W. H. Strange, R. R. |
| Copyright Year | 1982 |
| Description | Various configurations of high temperature, heat flux sensors were studied to determine their suitability for use in experimental combustor liners of advanced aircraft gas turbine engines. It was determined that embedded thermocouple sensors, laminated sensors, and Gardon gauge sensors, were the most viable candidates. Sensors of all three types were fabricated, calibrated, and endurance tested. All three types of sensors met the fabricability survivability, and accuracy requirements established for their application. |
| File Size | 14776930 |
| Page Count | 218 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830001774 |
| Archival Resource Key | ark:/13960/t7vm9316p |
| Language | English |
| Publisher Date | 1982-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Service Life Calibrating Thermocouples Temperature Probes Gas Turbine Engines Aircraft Engines Combustion Chambers Heat Flux Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
