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Test of a model propeller with symmetrical blade sections
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1926 |
| Description | This report, prepared at the request of NACA, gives the results of tests on a model propeller having blade sections with form of Gottingen airfoil no. 409. The model is shown to have a dynamic pitch practically equal to the nominal or geometrical pitch, and a somewhat higher efficiency but lower coefficient than would be expected of a propeller of more conventional sections. |
| File Size | 709900 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081061 |
| Archival Resource Key | ark:/13960/t57d62f7s |
| Language | English |
| Publisher Date | 1926-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propellers - Characteristics - Wind Tunnel Tests Airfoils - Goettingen 409-char ,propeller C P & Ordinates Propellers - Durand Wind Tunnel Tests Propeller - Wind Tunnel Tests 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 |
