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Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-propeller vtol model at static thrust
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1962 |
| Description | Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-propeller vtol model at static thrust |
| File Size | 4721818 |
| Page Count | 68 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19630000659 |
| Archival Resource Key | ark:/13960/t59d1p49w |
| Language | English |
| Publisher Date | 1962-12-01 |
| Access Restriction | Open |
| Subject Keyword | Static Thrust Vtol Aircraft Wing Pressure Distribution Slipstream Propeller 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 |