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Aerodynamic characteristics at reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the naca 0012 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 12824228 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082748 |
| Archival Resource Key | ark:/13960/t87h5xj6g |
| Language | English |
| Publisher Date | 1950-04-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Characteristics - Effect OF Surface Roughness Wind Tunnel Tests - Naca - Pressure, Low-turbulence Airfoils - Naca 0012 - Char , A C , Moments & Ordinates - Helicopter Airfoils - Characteristics - Effect OF Rivet Heads Airfoils - Characteristics -effect OF Trailing-edge Shape Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |