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Performance estimation for highly loaded six and ten blade propellers combined with an advanced technology turboshaft engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Morris Jr., S. J. |
| Copyright Year | 1980 |
| Description | Performance estimations, weights, and scaling laws for the six blade and ten blade highly loaded propellers combined with an advanced turboshaft engine are presented. These data are useful for aircraft mission studies using the turboprop system. Comparisons are made between the performance of post 1980 technology turboprop propulsion systems and the performance of both a current technology turbofan and a post 1990 technology turbofan. |
| File Size | 789494 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800019852 |
| Archival Resource Key | ark:/13960/t4xh4dn1x |
| Language | English |
| Publisher Date | 1980-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Turbofan Aircraft Turboprop Aircraft Propellers Propulsion System Performance Technological Forecasting Turboshafts Performance Prediction Turbofan Engines Air Breathing Engines Propeller Efficiency Turboprop Engines 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 |
