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Performance of an axial-flow compressor rotor designed for a pitch-section lift coefficient of 1.2
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 646557 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082024 |
| Archival Resource Key | ark:/13960/t50g80m3j |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Compressors, Axial Airfoils - Characteristics Effect OF Surface Roughness Rotor Blades - Pitch Loads - Rotors Lift Coefficients Airfoils - Rotor Blades Airfoils Surfaces - Roughness Compressors - Blades Blowers, Axial 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 |