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Dynamic gas temperature measurement system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Elmore, D. |
| Copyright Year | 1982 |
| Description | The development of an advanced measuring system which measures the rapidly varying gas temperature at the exit of an aircraft jet engine combustor during ground based testing of hot section components was identified. Sensor guidelines, technical approach/program schedule, and the accomplishments are reviewed. The environment of a present generation combustor is shown. The method uses two beadless junctions type-B thermocouples to measure heat transfer coefficient in situ. Heat conduction effects are shown by a finite element model of the thermocouple. |
| File Size | 315855 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850002650 |
| Archival Resource Key | ark:/13960/t1kh5dm1x |
| Language | English |
| Publisher Date | 1982-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Temperature Measurement Finite Element Method Conductive Heat Transfer Thermocouples Temperature Measuring Instruments High Temperature Gases Pyrometers Combustion Chambers Thermodynamic Properties Gas Temperature Heat Transfer Coefficients Turbine Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
