Loading...
Please wait, while we are loading the content...
Similar Documents
High-speed wind-tunnel tests of an naca 16-009 airfoil having a 32.9-percent-chord flap with an overhang 20.7 percent of the flap chord
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1947 |
| File Size | 17183992 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082028 |
| Archival Resource Key | ark:/13960/t49p7cr33 |
| Language | English |
| Publisher Date | 1947-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Naca - High-speed (2') Wing Flaps - Effect OF Gaps Airfoils - Characteristics - Effect OF Compressibility Airfoils - Naca 16-009 - Char & Moments - Wing Flaps Airfoils - Characteristics - Effect OF Surface Roughness Wing Flaps, Balanced Wing Flaps - Overhang 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 |