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Two-dimensional wind-tunnel investigation of the naca 64(sub 1)-012 airfoil equipped with two types of leading-edge flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 13767970 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081893 |
| Archival Resource Key | ark:/13960/t58d47r3h |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 641-012 - Char ,moments & Ordinates Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2 X 3') Work Carried On At Lal Airfoils - Characteristics - Effect OF Surface Roughness Wings - High Lift Devices Low-drag (wing Flaps) Wing Flaps, Split Wing Flaps, Leading-edge 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 |