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Experiments with a counter-propeller
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1933 |
| Description | This note describes tests made at Stanford University on a four-blade fixed counter-propeller in combination with a two-blade rotating propeller. It is shown that the efficiency of the normal form, well-designed air propeller can be increased about two percent over the full working range by the addition of fixed counter-propeller blades. |
| File Size | 8120022 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081275 |
| Archival Resource Key | ark:/13960/t55f20x1j |
| Language | English |
| Publisher Date | 1933-01-01 |
| Access Restriction | Open |
| Subject Keyword | 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 |