Loading...
Please wait, while we are loading the content...
Similar Documents
Low-speed investigation of the stalling of a thin, faired, double-wedge airfoil with nose flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 13150907 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082783 |
| Archival Resource Key | ark:/13960/t7hq88t0q |
| Language | English |
| Publisher Date | 1950-08-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils, Wedge - Double - Char & Moments Boundary Layer - Airfoils Wing Flaps, Leading-edge Pressure Distribution - Airfoils, Wedge - Double Stalling - Wings Wind Tunnel Tests - Aaf (10 Feet X 7 Feet) 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 |