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An experimental investigation of an naca 631-012 airfoil section with leading-edge suction slots
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 15382992 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082321 |
| Archival Resource Key | ark:/13960/t1fj6ss0q |
| Language | English |
| Publisher Date | 1948-08-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Airfoils - Naca 631-012 Wind Tunnel Tests - Aal (10'x7')(work Carried On At Aal) Boundary Layer Control - Airfoils - Naca 631-012 Boundary Layer Control - Suction - Slots Airfoils - Naca 631-012 - Char , Moments & Ordinates Airfoils - Naca 633-018 - Low-drag Low-drag (wing Slots & 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 |