Loading...
Please wait, while we are loading the content...
Similar Documents
Analyses of cooled turbine airfoil configurations at conditions of supersonic flight
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Analysis of first stage turbine stator vane and rotor blade cooling designs for application in highspeed aircraft |
| File Size | 3712183 |
| Page Count | 76 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710016879 |
| Archival Resource Key | ark:/13960/t5s80463v |
| Language | English |
| Publisher Date | 1969-04-01 |
| 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 |