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Cold-air investigation of a turbine with transpiration-cooled stator blades. 2 - stage performance with discrete hole stator blades
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1970 |
| Description | Cold air tests on axial flow turbine with transpiration cooled discrete hole stator blades to determine coolant flow ejection effect on turbine aerodynamic performance |
| File Size | 21028536 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710001535 |
| Archival Resource Key | ark:/13960/t3tt9cb75 |
| Language | English |
| Publisher Date | 1970-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |