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Single stage experimental evaluation of high mach number compressor rotor blading. part i - design of rotor blading
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1967 |
| Description | Axial-flow medium aspect ratio compressor rotor blade rows designed to evaluate use of blade camberline shape to minimize blade element losses at high transonic speed |
| File Size | 4906036 |
| Page Count | 83 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19670015749 |
| Archival Resource Key | ark:/13960/t7xm32909 |
| Language | English |
| Publisher Date | 1967-04-01 |
| Access Restriction | Open |
| Subject Keyword | Axial Flow Compressor Rotor Blade Transonic Speed 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 |