Loading...
Please wait, while we are loading the content...
Similar Documents
Experimental investigation of air-cooled turbine blade in turbojet engine viii : rotor blades with capped leading edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| Description | An air-cooled turbine blade with a capped leading edge was investigated in a modified commercial turbojet engine over a range of engine speed from 4000 to 11,350 rpm. The cooling performance of the caped-leading-edge configuration was superior to all leading-edge cooling modifications previously investigated. |
| File Size | 1006943 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930086862 |
| Archival Resource Key | ark:/13960/t9m375d00 |
| Language | English |
| Publisher Date | 1951-10-18 |
| Access Restriction | Open |
| Subject Keyword | Turbine Cooling Turbines - Blades - Temperature Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |