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Two-dimensional wind-tunnel investigation of an naca 64-009 airfoil equipped with two types of leading-edge flap
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 13795765 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082286 |
| Archival Resource Key | ark:/13960/t9k404b21 |
| Language | English |
| Publisher Date | 1948-06-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Leading-edge Wind Tunnel Tests - Naca - Pressure, Low-turbulence (7 1/2'x3') Work Carried On Airfoils - Naca 641-012 - Low-drag (wing Flaps) Airfoils - Characteristics - Effect OF Surface Roughness Airfoils - Naca 64-009 - Char , Moments & Ordinates Wing Flaps, Split Low-drag (wing Flaps) 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 |