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Rotor redesign for a highly loaded 1800 ft/sec tip speed fan. 1: aerodynamic and mechanical design report
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tari, U. Weber, R. M. Norton, J. M. |
| Copyright Year | 1979 |
| Description | A quasi three dimensional design system and multiple-circular-arc airfoil sections were used to design a fan rotor. An axisymmetric intrablade flow field calculation modeled the shroud of an isolated splitter and radial distribution. The structural analysis indicates that the design is satisfactory for evaluation of aerodynamic performance of the fan stage in a test facility. |
| File Size | 2673707 |
| Page Count | 102 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790017884 |
| Archival Resource Key | ark:/13960/t8cg4hq49 |
| Language | English |
| Publisher Date | 1979-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Test Facilities Compressor Rotors Aerodynamic Configurations Radial Distribution Airfoil Profiles Three Dimensional Flow Flow Distribution Pressure Distribution Mechanical Properties Quasi-steady States Tip Driven Rotors Structural Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
