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Jet-boundary corrections to the downwash behind powered models in rectangular wind tunnels with numerical values for 7- by 10-foot closed wind tunnels
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1942 |
| File Size | 1489871 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092661 |
| Archival Resource Key | ark:/13960/t43r42j79 |
| Language | English |
| Publisher Date | 1942-01-01 |
| Access Restriction | Open |
| Subject Keyword | Propeller Slipstream Lift - Airfoils Ground Effect - Wind Tunnel Tests, Image Vortices - Wings Pitching Moments Theories - Airfoils - Lifting-line Downwash Angles Elevators - Hinge Moments Wind Tunnels - Naca (10'x7') (amer ) 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 |