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The effects of high-lift devices on the low-speed stability of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| Description | Contains results of tunnel tests to determine effects of various combinations of split flaps, slats, and nose slats on the stability characteristics of a tapered 37.5 degree sweptback wing of aspect ratio 3 in straight and rolling flow. |
| File Size | 13683826 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085527 |
| Archival Resource Key | ark:/13960/t2s510m4k |
| Language | English |
| Publisher Date | 1948-11-09 |
| Access Restriction | Open |
| Subject Keyword | Slots AND Slats - Complete Wings Flaps - Complete Wings Stability, Directional - Static Stability, Lateral - Static Damping Derivatives - Stability Sweep - Complete Wings 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 |