Loading...
Please wait, while we are loading the content...
Similar Documents
Investigation in the langley 19-foot pressure tunnel of two wings of naca 65-210 and 64-210 airfoil sections with various type flaps (Document No: 19930082231)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 3860246 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082231 |
| Archival Resource Key | ark:/13960/t0zp8c86f |
| Language | English |
| Publisher Date | 1948-05-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Split Wing Flaps, Slotted Airfoils - Characteristics Effect OF Surface Roughness Wind Tunnel Tests - Naca - Pressure (19') Airfoils-naca 65-210-char , Moments & Ordinates Wing Flaps Wing Flaps, Slotted - Double Airfoils-naca 64-210-char , Moments & Ordinages Wing Flaps Interferenc E- Wings & Fuselages 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 |