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Pressure-loss and flow coefficients inside a chordwise-finned, impingement, convection, and film air-cooled turbine vane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hippensteele, S. A. |
| Copyright Year | 1974 |
| Description | Total-pressure-loss coefficients, flow discharge coefficients, and friction factors were determined experimentally for the various area and geometry changes and flow passages within an air-cooled turbine vane. The results are compared with those of others obtained on similar configurations, both actual and large models, of vane passages. The supply and exit air pressures were controlled and varied. The investigation was conducted with essentially ambient-temperature air and without external flow of air over the vane. |
| File Size | 1013305 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740011532 |
| Archival Resource Key | ark:/13960/t0zp8sx6x |
| Language | English |
| Publisher Date | 1974-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbomachine Blades Air Flow Air Cooling Pressure Distribution Aerodynamic Coefficients Flow Geometry Heat Transfer Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
