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Effects of modifications to the leading-edge region on the stalling characteristics of the naca 63(sub 1)-012 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 967658 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082866 |
| Archival Resource Key | ark:/13960/t9x10fb0v |
| Language | English |
| Publisher Date | 1950-11-01 |
| Access Restriction | Open |
| Subject Keyword | Wings Flaps, Leading-edge Pressure Distribution - Airfoils - Naca 63 Sub 1-012 Stalling - Wings Airfoils - Naca 63 Sub 1-012 - Char , Moments & Ordinates Wind Tunnel Tests - Aal (10'x7', No 1) Wings - Leading Edges 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 |