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Dependence of propeller efficiency on angle of attack of propeller blade
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1921 |
| Description | In order to determine the maximum and the most favorable pitch for a propeller, it was found desirable to investigate the dependence of propeller efficiency on the angle of attack of the propeller blade. The results of a few experiments are given to show that propeller blades conduct themselves just like airplane wings with reference to the dependence of their efficiency on their angle of attack. |
| File Size | 257194 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930080772 |
| Archival Resource Key | ark:/13960/t9477k628 |
| Language | English |
| Publisher Date | 1921-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propellers - Efficiency Propellers, Experiments 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 |
