Loading...
Please wait, while we are loading the content...
Similar Documents
Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular naca 23012 airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1941 |
| File Size | 22397525 |
| Page Count | 47 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092827 |
| Archival Resource Key | ark:/13960/t4tj1q87w |
| Language | English |
| Publisher Date | 1941-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wing Flaps, Split - Perforated Air Flow - Wakes Wing Flaps, Split - Double (perforated) Airfoils - Naca 23012 - Char & Moments - Wing Flaps, Split (double) (perforated Airfoils - Naca 23012 - Char & Moments - Wing Flaps, Split (perforated) Wing Flaps, Dive-control 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 |